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		<id>https://wiki.oldengin.es/index.php?title=High-Speed_High-Output_Diesel_Engines&amp;diff=901</id>
		<title>High-Speed High-Output Diesel Engines</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;== High-Speed High-Output Diesel Engines - 35 Years of Development of Railroad and Marine Applications ==&lt;br /&gt;
By Markus von Kienlin and G. W. Maybach &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;History&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
TO THE EXPERT, the name of Maybach Motorenbau immediately recalls a special class of engines characterized by the following outstanding features: high speed, light weight, small size, high fatigue strength (due to special design and production measures,) and low operating cost. &lt;br /&gt;
&lt;br /&gt;
The unique development of the Zeppelin airship after the historic accident at Echterdingen in 1908, was decisively governed by the fact that Wilhelm Maybach, Gottlieb Daimler&#039;s collaborator, made available to Count Zeppelin an engine designed by his son, Karl Maybach. This was a 6-cyl 150 hp 1200 rpm engine with a fuel consumption of 254 g/hph and a weight-to-power ratio of no more than 2,99 kg/hp, in contrast to the engine installed in the first Zeppelin airship which had a weight of 26 kg/hp and a consumption of 508 g/hph. For the production of the new engine, Count Zeppelin and Wilhelm Maybach founded, on March 23, 1909, the Luftfahrzeug-Motorenbau G.m.b.H. which was affilleated to Luftschiffbau Zeppelin. The Maybach Motorenbau, which was entrusted to Karl Maybach from the outset, produced the engines for further Zeppelin airships and for aeroplanes. Among those engines, as early as 1917, highly rated high-compression high-altitude engines were built. Fig. 1 shows such a high-altitude aircraft engine. Fig. 2 is a sectional view of the cylinder liner and wrist pin area.&lt;br /&gt;
&lt;br /&gt;
After the enforced interruption of almost the entire production at the end of World War I, new and related lines of production suitable for the skilled staff had to be found. The choice included Otto and diesel engines for a number of purposes. Research continued on Zeppelin airship engines including the well-known 550 hp VL-type engine (Fig. 3) for the airship &amp;quot;Graf Zeppelin,&amp;quot; which accomplished the famous world tours under the command of the late Dr. Eckener, who until his death in 1954 was chairman of the Maybach Motorenbau. The first powerful high-speed diesel engine was developed in the Maybach workshops between 1919 and 1923. Construction of this G 4 engine (Fig. 4) was a remarkable   venture, bearing in mind that at that time experience with high-speed diesel engines was actually only with submarine engines having a maximum speed of not more than 500 rpm, whereas the new 150 hp Maybach diesel engine had an operating speed of 1300 rpm.&lt;br /&gt;
&lt;br /&gt;
Solid fuel injection was then still at its beginning, so that the G 4 engine had air injection. Fig. 4 shows the relative sizes of the diesel engine and the engine-driven air compressor needed for air injection. &lt;br /&gt;
&lt;br /&gt;
Opinion at that time - which many still hold today - was that the high-speed engines despite their obvious advantages with respect to weight and reduced space requirements would have a shorter service life, have less favorable consumption figures, and be more prone to trouble. This opinion chiefly resulted from the fact that many firms tried to increase the output of their existent low-speed engines merely by increasing the engine speed and neglecting any improvements in design. Naturally, this led to setbacks which in turn gave rise to such widespread opinion. The Maybach Motorenbau, which even then had many years of experience in the field of high-speed Otto engines, adopted new methods by designing a diesel engine especially for high speed and by aiming simultaneously at a corresponding increase of operating reliability and service life, two requirements obviously necessary for airship engines.&lt;br /&gt;
&lt;br /&gt;
Since the first results with high-speed diesel engines were very encouraging, the development of these engines was continued and their output increased. The output of the first 6-cyl engine was soon raised to 210 hp at 1400 rpm. followed in 1930 by a 12-cyl V-engine providing 410 hp at 1400 rpm which, at a later date, was brought to 600 and 650 hp by exhaust gas supercharging (Fig. 5). In 1931 two of these 410 hp GO 5 engines were installed in the &amp;quot;Fliegender Hamburger,&amp;quot; the first high-speed railcar-train of the German State Railway (Fig, 6). Its schedule speed of 77.6 mph, no less than the regular daily top speed of 100 mph, on the route between Hamburg and Berlin was a sensation at the time among railroad experts. &lt;br /&gt;
&lt;br /&gt;
These Maybach engines of the GO-type - primarily designed as power units for railcars - set the fashion for diesel train operation of this power class in Europe until the year 1940. Hundreds of railcars and diesel trains were equipped with these engines in Germany, France, Belgium, Holland, Sweden, Norway, and Spain. Moreover, the engines met with favorable reception in naval construction, and were increasingly used for high-speed passenger boats, customs cruisers, yachts, coastguard crafts, and other craft. &lt;br /&gt;
&lt;br /&gt;
The GO-type were designed so that the cylinder blocks of 6.30 in. bore and 7.88 in. stroke, made in one casting with the cylinder head, were assembled in an aluminum crankcase. The engines had direct injection, and four valves per cylinder controlled by overhead camshafts.&lt;br /&gt;
&lt;br /&gt;
tons were made of aluminum. Convenient mounting of running parts posed a special problem at the time for these pow-&lt;br /&gt;
&lt;br /&gt;
White metal bearings could not be used, and&lt;br /&gt;
&lt;br /&gt;
lead-bronze bearings were still in too early stages of develop-&lt;br /&gt;
&lt;br /&gt;
ment. Therefore, it was decided to provide both the crank-&lt;br /&gt;
&lt;br /&gt;
shaft and big ends with roller bearings, the composition of&lt;br /&gt;
&lt;br /&gt;
material and thermal treatment for which were the subject&lt;br /&gt;
&lt;br /&gt;
of lengthy and painstaking development by the company.&lt;br /&gt;
&lt;br /&gt;
In operation, these engines attained mileages between&lt;br /&gt;
&lt;br /&gt;
general overhauls of as much as 100,000 miles (about 2500 operating hours) and more, which prior to World War I was&lt;br /&gt;
&lt;br /&gt;
regarded as quite satisfactory.&lt;br /&gt;
&lt;br /&gt;
After termination of World War Il the situation was en-&lt;br /&gt;
&lt;br /&gt;
tirely different. Under the influence of the immense ad-&lt;br /&gt;
&lt;br /&gt;
vance of the diesel locomotive in the United States and else-&lt;br /&gt;
&lt;br /&gt;
where, railway companies became increasingly interested&lt;br /&gt;
&lt;br /&gt;
in converting their heavy traction service to diesel operation.&lt;br /&gt;
&lt;br /&gt;
If European manufacturers wanted to take part in this de-&lt;br /&gt;
&lt;br /&gt;
velopment, they had to counter the American diesel lo-&lt;br /&gt;
&lt;br /&gt;
comotive with its heavy and slow-running engine by a type&lt;br /&gt;
&lt;br /&gt;
of vehicle which would be available for a more universal&lt;br /&gt;
&lt;br /&gt;
application, offer more favorable weight conditions, and&lt;br /&gt;
&lt;br /&gt;
which in respect of output and service life would at least&lt;br /&gt;
&lt;br /&gt;
equal the heavy engines.&lt;br /&gt;
&lt;br /&gt;
For Maybach Motorenbau, as the representative of the&lt;br /&gt;
&lt;br /&gt;
European trend, the demand for long life of the engine and&lt;br /&gt;
&lt;br /&gt;
components became&lt;br /&gt;
&lt;br /&gt;
small-size engines had to be designed which would be cap-&lt;br /&gt;
&lt;br /&gt;
able of offering mileages between overhauls at least equal&lt;br /&gt;
&lt;br /&gt;
to those then attained in rail traction by the finest types of&lt;br /&gt;
&lt;br /&gt;
slow-speed engines. Beyond that, these engines were sup-&lt;br /&gt;
&lt;br /&gt;
posed not only to compete successfully in the field of diesel&lt;br /&gt;
&lt;br /&gt;
traction, but also to conquer new fields of application.&lt;br /&gt;
&lt;br /&gt;
Considering that for the aforementioned GO-type engines&lt;br /&gt;
&lt;br /&gt;
the roller bearings in the big end of the connecting rods were&lt;br /&gt;
&lt;br /&gt;
the limiting factor for the running performance, it was ob-&lt;br /&gt;
&lt;br /&gt;
vious that further development should aim at plain bearings&lt;br /&gt;
&lt;br /&gt;
for the big ends and a modernization of all running parts.&lt;br /&gt;
&lt;br /&gt;
The best solution in this direction appeared to be the disc-&lt;br /&gt;
&lt;br /&gt;
webbed crankshaft, which inherently has greatly improved&lt;br /&gt;
&lt;br /&gt;
vibration characteristics, and which also provides ideal con-&lt;br /&gt;
&lt;br /&gt;
ditions for the entire bearing problem.&lt;br /&gt;
&lt;br /&gt;
This was confirmed by the experience gained by May-&lt;br /&gt;
&lt;br /&gt;
bach Motorenbau during the last war with more than 50,000&lt;br /&gt;
&lt;br /&gt;
Otto engines ranging from 300 to 700 hp at 3000 rpm, equip-&lt;br /&gt;
&lt;br /&gt;
ped with disc-webbed crankshafts and installed in heavy-&lt;br /&gt;
&lt;br /&gt;
duty military vehicles (tanks and heavy trucks).a s a m a t e r&lt;br /&gt;
&lt;br /&gt;
of fact, the adaptation of the disc-webbed crankshaft to the&lt;br /&gt;
&lt;br /&gt;
aforementioned pre-war GO-type, resulted in the change-over to the so-called GTO-&amp;quot;tunnel&amp;quot; type crankcase, repre-&lt;br /&gt;
&lt;br /&gt;
senting a unique jump ahead in development.&lt;br /&gt;
&lt;br /&gt;
Proof of this was the service results achieved by the Ger-&lt;br /&gt;
&lt;br /&gt;
man Federal Railway with its 600 bhp Maybach GTO type&lt;br /&gt;
&lt;br /&gt;
tunnel engines. It was revealed by spot checks that the bear-&lt;br /&gt;
&lt;br /&gt;
ings of these engines operating at 1400 rpm were still like&lt;br /&gt;
&lt;br /&gt;
new after distances of 300,000-400,000 miles. All other&lt;br /&gt;
&lt;br /&gt;
wearing parts showed such slight wear that a general over-&lt;br /&gt;
&lt;br /&gt;
haul was not anticipated before 600,000-700,000 miles, cor-&lt;br /&gt;
&lt;br /&gt;
responding to about 12,000 to 15,000 operating hr. Early&lt;br /&gt;
&lt;br /&gt;
in 1955, these 600 bhp engines had exceeded an aggregate&lt;br /&gt;
&lt;br /&gt;
mileage of more than 6 million miles without any major en-&lt;br /&gt;
&lt;br /&gt;
gine overhauls (1).*&lt;br /&gt;
&lt;br /&gt;
Today there are more than 1000 of these 12-cyl GTO en-&lt;br /&gt;
&lt;br /&gt;
gines rated up to 800 hp in service. Of these 840 are in-&lt;br /&gt;
&lt;br /&gt;
stalled in shunting locomotives of the European standard type&lt;br /&gt;
&lt;br /&gt;
V.60, running for 20,000-25,000 hr before a piston check&lt;br /&gt;
&lt;br /&gt;
is scheduled.&lt;br /&gt;
&lt;br /&gt;
Thus an optimum solution was found for the problems pre-&lt;br /&gt;
&lt;br /&gt;
sented by the running gear of this engine type. For more&lt;br /&gt;
&lt;br /&gt;
powerful engines, however, with continuous outputs of about&lt;br /&gt;
&lt;br /&gt;
100 hp per cylinder and with similar or rather better service&lt;br /&gt;
&lt;br /&gt;
behavior, one more step was necessary. That step was the&lt;br /&gt;
&lt;br /&gt;
introduction of the tunnel construction with roller main bear-&lt;br /&gt;
&lt;br /&gt;
The performance of this&lt;br /&gt;
&lt;br /&gt;
was proved first by thorough trials with powerful diesel en-&lt;br /&gt;
&lt;br /&gt;
gines of a speed range between 2400 and 2600 rpm. Even-&lt;br /&gt;
&lt;br /&gt;
tually this led to the present Maybach MD tunnel engine,&lt;br /&gt;
&lt;br /&gt;
a design which has aroused great interest in the technical&lt;br /&gt;
&lt;br /&gt;
world. With this design, the problem of building a high-&lt;br /&gt;
&lt;br /&gt;
speed diesel engine with a running performance equal to,&lt;br /&gt;
&lt;br /&gt;
of better than that of a good slow-speed engine, can be re-&lt;br /&gt;
&lt;br /&gt;
garded as solved.&lt;br /&gt;
&lt;br /&gt;
Before giving a more detailed description of the MD de-&lt;br /&gt;
&lt;br /&gt;
sign, it may be advantageous to discuss some general prob-&lt;br /&gt;
&lt;br /&gt;
lems pertaining to high engine speed, and to report on the&lt;br /&gt;
&lt;br /&gt;
research techniques which contributed essentially to the de-&lt;br /&gt;
&lt;br /&gt;
velopment of the modern Maybach diesel engines.&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;General Questions Relating to High Engine Speed&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
It is, first of all, necessary to emphasize a fact often&lt;br /&gt;
&lt;br /&gt;
insufficiently realized by users: engine speed alone does not&lt;br /&gt;
&lt;br /&gt;
provide an adequate criterion for the genuine high-speed&lt;br /&gt;
&lt;br /&gt;
character of an engine. Even the mean piston speed does&lt;br /&gt;
&lt;br /&gt;
not provide such a criterion, since the mean effective pres-&lt;br /&gt;
&lt;br /&gt;
sure must also be taken into account, as well as whether the&lt;br /&gt;
&lt;br /&gt;
piston speed is used with high or low mean effective pressure&lt;br /&gt;
&lt;br /&gt;
at equal engine speed.&lt;br /&gt;
&lt;br /&gt;
Some performance characteristics, important as far as&lt;br /&gt;
&lt;br /&gt;
engine loading is concerned, are now considered. Besides&lt;br /&gt;
&lt;br /&gt;
the absolute engine power N and the specific power per cyl-&lt;br /&gt;
&lt;br /&gt;
inder N/z, it is quite common to use the ratio of power per&lt;br /&gt;
&lt;br /&gt;
unit of swept volume N/V, characterizing the degree of util-ization of the swept volume. The ratio of power per unit&lt;br /&gt;
&lt;br /&gt;
of piston area, N/F, also has a bearing in this connection:&lt;br /&gt;
&lt;br /&gt;
it signifies the total engine power related to the total area&lt;br /&gt;
&lt;br /&gt;
of the piston crowns. The piston crown is one of the engine&lt;br /&gt;
&lt;br /&gt;
parts subjected to the highest thermal load. To dissipate&lt;br /&gt;
&lt;br /&gt;
the heat accumulated here by means of conduction, radia-&lt;br /&gt;
&lt;br /&gt;
tion, or coolants is a matter of vital importance which may&lt;br /&gt;
&lt;br /&gt;
well be a limiting factor in increasing the specific engine&lt;br /&gt;
&lt;br /&gt;
power.&lt;br /&gt;
&lt;br /&gt;
Strictly speaking, the ratios of power per unit of displaced&lt;br /&gt;
&lt;br /&gt;
volume, and power per unit of piston area can only pro-&lt;br /&gt;
&lt;br /&gt;
vide a valid scale of comparison if the cylinders compared&lt;br /&gt;
&lt;br /&gt;
have the same size and shape. The influence of the stroke-&lt;br /&gt;
&lt;br /&gt;
to-bore ratio on these parameters has been investigated by&lt;br /&gt;
&lt;br /&gt;
Jaklitsch (2). Under certain limiting assumptions, he found&lt;br /&gt;
&lt;br /&gt;
that this influence is of the order of Vs/d, (s = stroke d =&lt;br /&gt;
&lt;br /&gt;
bore) a result derived statistically for diesel engines designed&lt;br /&gt;
&lt;br /&gt;
for aircraft and road vehicles, and it may be assumed, that&lt;br /&gt;
&lt;br /&gt;
this influence is equally applicable to larger types of diesel&lt;br /&gt;
&lt;br /&gt;
engines.&lt;br /&gt;
&lt;br /&gt;
The fact that the ratio of power per unit of swept vol-&lt;br /&gt;
&lt;br /&gt;
ume is influenced by the stroke-to-bore ratio can be ex-&lt;br /&gt;
&lt;br /&gt;
plained by the fact that as this ratio changes there is also&lt;br /&gt;
&lt;br /&gt;
a change in the ratio of the heat-affected surface to the cor-&lt;br /&gt;
&lt;br /&gt;
responding swept volume. With the longer stroke engine,&lt;br /&gt;
&lt;br /&gt;
where the piston diameter is smaller, the distance of heat&lt;br /&gt;
&lt;br /&gt;
flow from the center of the piston crown to the cylinder wal&lt;br /&gt;
&lt;br /&gt;
is smaller. Therefore, the temperatures at the center of&lt;br /&gt;
&lt;br /&gt;
the piston crown become higher if the piston diameter is&lt;br /&gt;
&lt;br /&gt;
increased. The results of similar investigations on the in-&lt;br /&gt;
&lt;br /&gt;
fluence of cylinder bore and stroke-to-bore ratio on the piston&lt;br /&gt;
&lt;br /&gt;
temperature are plotted in Fig. 7. This graph shows that,&lt;br /&gt;
&lt;br /&gt;
even if mean effective pressure, piston speed, and stroke-&lt;br /&gt;
&lt;br /&gt;
to-bore ratio remain constant, an increase in the cylinder&lt;br /&gt;
&lt;br /&gt;
bore causes higher temperatures at the center of the piston&lt;br /&gt;
&lt;br /&gt;
crown. It will also be noted that the increase is steeper with&lt;br /&gt;
&lt;br /&gt;
short-stroke engines than with long-stroke engines. In order&lt;br /&gt;
&lt;br /&gt;
to obtain more realistic parameters for comparisons, the ratios of power per unit of swept volume and power per unit of piston area must be related to the stroke-to-bore ratio &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Apart from having such parameters as the specific power-to-volume ratio, and the specific power-to-piston area ratio, which are more indicative of the thermal loading of the pistons, it is also of importance to obtain criteria characterizing the mechanical stresses occurring in the rotating crankshaft assembly. This applies in particular to the big-end bearings, the loading of which might be characterized by the mass forces of the rotating and oscillating parts of the engine as well as by the maximum gas pressure. Assuming that, with the application of corresponding design principles, the weights of the rotating and oscillating engine parts vary with the third power of the piston diameter, a parameter a can be formed relating the mass forces to the unit of piston area, for example:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Jaklitsch calls this a value &amp;quot;running index&amp;quot; (2), and as-&lt;br /&gt;
&lt;br /&gt;
cribes to it a major importance. The term &amp;quot;mass-force fac-&lt;br /&gt;
&lt;br /&gt;
tor,&amp;quot; however, appears to be more suitable as it relates more&lt;br /&gt;
&lt;br /&gt;
directly to the significance of the parameter. F o r i t i t 1s&lt;br /&gt;
&lt;br /&gt;
accepted that, with a corresponding utilization of the cyl-&lt;br /&gt;
&lt;br /&gt;
inder diameter, the projected area of the big-end bearings&lt;br /&gt;
&lt;br /&gt;
increases with the square of the piston diameter, the mass-&lt;br /&gt;
&lt;br /&gt;
force factor may well be accepted as a valid criterion for&lt;br /&gt;
&lt;br /&gt;
the bearing load due to the mass forces.&lt;br /&gt;
&lt;br /&gt;
If the two engines compared are geometrically similar,&lt;br /&gt;
&lt;br /&gt;
that is, if the stroke-to-bore ratio remains the same, the&lt;br /&gt;
&lt;br /&gt;
above assumption is strictly true, as the masses in motion&lt;br /&gt;
&lt;br /&gt;
do vary with the third power of the piston diameter. In order&lt;br /&gt;
&lt;br /&gt;
to gain an idea in regard to the variation of the masses act-&lt;br /&gt;
&lt;br /&gt;
ing the big-end b e a r i n g W h e n t e s t o k e - t o - b o r e t a l l o&lt;br /&gt;
&lt;br /&gt;
is modified, this ratio was altered in a V-engine and the&lt;br /&gt;
&lt;br /&gt;
variation of the masses acting on the bearing was calculated.&lt;br /&gt;
&lt;br /&gt;
It was found that when the stroke-to-bore ratio was increased&lt;br /&gt;
&lt;br /&gt;
by as much as 60% the increase in weight was no more&lt;br /&gt;
&lt;br /&gt;
than 2-3%. It follows that, within reasonable limits, the&lt;br /&gt;
&lt;br /&gt;
mistake made by assuming that the variation of masses is&lt;br /&gt;
&lt;br /&gt;
proportional to d3 is insignificant.&lt;br /&gt;
&lt;br /&gt;
F r o m this may be concluded that the engine with the&lt;br /&gt;
&lt;br /&gt;
most efficiently utilized crankshaft is the one which has the&lt;br /&gt;
&lt;br /&gt;
highest mass-force factor a, and, at the same time, can&lt;br /&gt;
&lt;br /&gt;
prove to be reliable in service and to have the service life&lt;br /&gt;
&lt;br /&gt;
expected for its application (5).&lt;br /&gt;
&lt;br /&gt;
The diagram in Fig. 8 is intended to show the signifi-&lt;br /&gt;
&lt;br /&gt;
cance of the mass-force factor. For instance, if an engine has a speed of 1300 rpm and a cylinder bore of 7.28 in.,&lt;br /&gt;
&lt;br /&gt;
with a stroke of 7.78 in. the mass-force factor becomes 672&lt;br /&gt;
&lt;br /&gt;
ft/min?. If the same engine is accelerated to 1800 rpm, the&lt;br /&gt;
&lt;br /&gt;
mass-force factor increases to 1289 ft/min?. With a slow-&lt;br /&gt;
&lt;br /&gt;
speed engine of, say, 250 rpm, 17.72 in. bore and 25.58&lt;br /&gt;
&lt;br /&gt;
in. stroke, the mass-force factor is no greater than 199 ft?/&lt;br /&gt;
&lt;br /&gt;
min?. Since both slow-speed and high-speed engines under&lt;br /&gt;
&lt;br /&gt;
consideration have actually been found to be very reliable&lt;br /&gt;
&lt;br /&gt;
in practice, it follows that the crankshaft assembly of the&lt;br /&gt;
&lt;br /&gt;
high-speed engine is much more efficiently utilized than&lt;br /&gt;
&lt;br /&gt;
that of the slow-speed engine.&lt;br /&gt;
&lt;br /&gt;
In order to explain the significance of the mass-force fac-&lt;br /&gt;
&lt;br /&gt;
tor still more in detail the characteristic parameters have&lt;br /&gt;
&lt;br /&gt;
been determined for some of the most important present-&lt;br /&gt;
&lt;br /&gt;
time locomotive engines of about 1000 bhp and more. The&lt;br /&gt;
&lt;br /&gt;
data are listed in Table 1. Four-cycle engines have been&lt;br /&gt;
&lt;br /&gt;
selected only so as to make a simple comparison of the par-&lt;br /&gt;
&lt;br /&gt;
ameters possible.&lt;br /&gt;
&lt;br /&gt;
Two engines with equal characteristic parameters can&lt;br /&gt;
&lt;br /&gt;
be assumed to show equal service performance of their pis-&lt;br /&gt;
&lt;br /&gt;
ton and crankshaft assemblies. This, however, holds only&lt;br /&gt;
&lt;br /&gt;
for engines of similar design. Therefore the parameters&lt;br /&gt;
&lt;br /&gt;
should never be compared on their own, but only under sim-&lt;br /&gt;
&lt;br /&gt;
ultaneous consideration of the designs of the engines involved.&lt;br /&gt;
&lt;br /&gt;
It appears from Table 1 that the specific power-to-piston&lt;br /&gt;
&lt;br /&gt;
area ratio of the locomotive engines - irrespective of their&lt;br /&gt;
&lt;br /&gt;
power and speed - is within the limits 210 to 345 bhp/ft?,&lt;br /&gt;
&lt;br /&gt;
excluding the engines represented by items 8 and 9, which will be discussed later. For the turbocharged stationary en-&lt;br /&gt;
&lt;br /&gt;
gines, rated at continuous speeds from 250 to 600 rpm, the&lt;br /&gt;
&lt;br /&gt;
respective p o w e r - t o - p i s t o n a r e a r a t i o s r a n g e a p p r o x i m a t e l y&lt;br /&gt;
&lt;br /&gt;
between 93 and 186 bhp/ft?. From this comparison it be-&lt;br /&gt;
&lt;br /&gt;
comes quite evident that the effort to ensure small bulk of&lt;br /&gt;
&lt;br /&gt;
the locomotive engines to make them suitable for their ap-&lt;br /&gt;
&lt;br /&gt;
plication, imposes high demands on engine design as well&lt;br /&gt;
&lt;br /&gt;
as on material when operational reliability and life of the&lt;br /&gt;
&lt;br /&gt;
wearing parts of both engine groups is to be the same. Even&lt;br /&gt;
&lt;br /&gt;
more revealing are here the high mass-force factors for the&lt;br /&gt;
&lt;br /&gt;
locomotive engines which range between 603 and 915 f t /&lt;br /&gt;
&lt;br /&gt;
min&#039;, whereas the corresponding figures for stationary en-&lt;br /&gt;
&lt;br /&gt;
gines lie only between 215 and 431 ft ⅔ /min?.&lt;br /&gt;
&lt;br /&gt;
These simple considerations show that locomotive en-&lt;br /&gt;
&lt;br /&gt;
gines which have proved satisfactory in practical operation&lt;br /&gt;
&lt;br /&gt;
must be types of a highly meritorious design, for they have&lt;br /&gt;
&lt;br /&gt;
withstood the imposition of quite severe demands.&lt;br /&gt;
&lt;br /&gt;
In order to permit a comparison between different en-&lt;br /&gt;
&lt;br /&gt;
gines on the basis of the criteria developed above, a com-&lt;br /&gt;
&lt;br /&gt;
mon basis of &amp;quot;equal loading&amp;quot; has to be defined. &amp;quot;Equal&lt;br /&gt;
&lt;br /&gt;
loading&amp;quot; of two engines specifically means that the mech-&lt;br /&gt;
&lt;br /&gt;
anical and thermal loading of piston and crankshaft assem-&lt;br /&gt;
&lt;br /&gt;
blies of the two engines is the same. This is characterized&lt;br /&gt;
&lt;br /&gt;
by: &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
The conception of geometric similarity is understood to&lt;br /&gt;
&lt;br /&gt;
cover not only the cylinders, (stroke and bore), but also all&lt;br /&gt;
&lt;br /&gt;
those parts of the engine which are subjected to any stresses.&lt;br /&gt;
&lt;br /&gt;
In all these comparisons, the mechanical efficiencies of the&lt;br /&gt;
&lt;br /&gt;
engines are assumed to be constant.&lt;br /&gt;
&lt;br /&gt;
From the well-known engine power equation:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Assuming that for two geometrically similar engines (s/d =&lt;br /&gt;
&lt;br /&gt;
constant) the mean piston speed Cm the mean effective&lt;br /&gt;
&lt;br /&gt;
pressure Po, the swept volume Ve and the ratio N/ are&lt;br /&gt;
&lt;br /&gt;
constant, the correlation between power and number of cyl-&lt;br /&gt;
&lt;br /&gt;
inders becomes:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Fig. 9 shows this functional relationship indicative of the&lt;br /&gt;
&lt;br /&gt;
increase in output obtained with an engine of the same total&lt;br /&gt;
&lt;br /&gt;
swept volume by increasing the number of cylinders.&lt;br /&gt;
&lt;br /&gt;
For instance, if a plant hitherto driven by one slow-speed&lt;br /&gt;
&lt;br /&gt;
12-cyl engine is driven, instead, by eight high-speed 12-&lt;br /&gt;
&lt;br /&gt;
cyl engines which have altogether the same total swept vol-&lt;br /&gt;
&lt;br /&gt;
ume as the one slow-speed engine, the output is doubled&lt;br /&gt;
&lt;br /&gt;
although mechanical and thermal stresses in the piston and&lt;br /&gt;
&lt;br /&gt;
crankshaft assembly are the same. If it were intended to&lt;br /&gt;
&lt;br /&gt;
achieve this doubling of output by enlarging the swept vol-&lt;br /&gt;
&lt;br /&gt;
ume of the single slow-speed engine, the swept volume of&lt;br /&gt;
&lt;br /&gt;
that engine would have to be increased 2.8 times.&lt;br /&gt;
&lt;br /&gt;
Finally, regarding the significance of the parameter of&lt;br /&gt;
&lt;br /&gt;
specific power output per unit of piston area as a factor char-&lt;br /&gt;
&lt;br /&gt;
acterizing engine loading, it may be used to divide engines&lt;br /&gt;
&lt;br /&gt;
into different load or performance categories. For instance&lt;br /&gt;
&lt;br /&gt;
certain ranges of this specific power-to-piston area factor&lt;br /&gt;
&lt;br /&gt;
can be assigned to the category of engines of high specific&lt;br /&gt;
&lt;br /&gt;
output, to the category of vehicle engines, the category of&lt;br /&gt;
&lt;br /&gt;
marine engines, and so on. Under these assumptions can&lt;br /&gt;
&lt;br /&gt;
be derived for N/F/Vs/d = constant and (s/d) = const.: &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
for a given load category and geometrically similar engines,&lt;br /&gt;
&lt;br /&gt;
the specific power-to-swept volume ratio is inversely pro-&lt;br /&gt;
&lt;br /&gt;
portional to the bore.&lt;br /&gt;
&lt;br /&gt;
Fig. 10 shows the relationship between the specific pow-&lt;br /&gt;
&lt;br /&gt;
er-to-swept volume factor and the bore for different values&lt;br /&gt;
&lt;br /&gt;
of the specific power-to-piston area factor. For example,&lt;br /&gt;
&lt;br /&gt;
with geometrically similar engines of equal thermal and mechanical stressing of their piston resp, crankshaft assemblies,&lt;br /&gt;
&lt;br /&gt;
the doubling of the bore would halve the power per unit&lt;br /&gt;
&lt;br /&gt;
swept volume. In the same figure data are plotted for four&lt;br /&gt;
&lt;br /&gt;
high-speed engines belonging to four different performance&lt;br /&gt;
&lt;br /&gt;
categories, and one slow-speed marine propulsion engine.&lt;br /&gt;
&lt;br /&gt;
The data of these engines are listed in Table 2.&lt;br /&gt;
&lt;br /&gt;
Table 2 shows that a normal high-speed engine (for ex-&lt;br /&gt;
&lt;br /&gt;
ample, Engine No. 1) has the same power output per unit&lt;br /&gt;
&lt;br /&gt;
of piston area as the slow-speed marine engine No. 5, where&lt;br /&gt;
&lt;br /&gt;
the power of the latter must be regarded as being rather high&lt;br /&gt;
&lt;br /&gt;
compared with other similar engines. With high-speed en-&lt;br /&gt;
&lt;br /&gt;
gines, however, by means of suitable measures such as pis-&lt;br /&gt;
&lt;br /&gt;
ton cooling the specific power output per unit of piston area&lt;br /&gt;
&lt;br /&gt;
can be increased for marine engines to 304 bhp/ft?, as shown&lt;br /&gt;
&lt;br /&gt;
for No. 3 engine. Yet this still does not exhaust the possi-&lt;br /&gt;
&lt;br /&gt;
bilities of increasing the specific power output. As No. 4&lt;br /&gt;
&lt;br /&gt;
engine shows, by an increase in speed, mean effective pres-&lt;br /&gt;
&lt;br /&gt;
sure, and by other measures, the specific power-to-piston&lt;br /&gt;
&lt;br /&gt;
area factor of the same engine can be raised to beyond 600 bhp/ft?, a value which cannot be approached even remotely&lt;br /&gt;
&lt;br /&gt;
by slow-speed engines. This comparison clearly demonstrates&lt;br /&gt;
&lt;br /&gt;
the possibilities for high-speed engines to increase their spe-&lt;br /&gt;
&lt;br /&gt;
cific power output; it also demonstrates the wide power range&lt;br /&gt;
&lt;br /&gt;
which can be obtained with one and the same engine.&lt;br /&gt;
&lt;br /&gt;
The higher the specific power-to-piston area factor is of an engine which has proved to be reliable in actual service, the higher is the standard of technical development which the particular engine can be said to have reached. Hereby the measures are quite decisive by means of which higher specific power output per unit piston area has been attained, without exerting a detrimental influence on the reliability of the engine.&lt;br /&gt;
&lt;br /&gt;
In the high-speed Maybach MD engines, a great step forward was made with the introduction of pressure-oil piston cooling . Fig. I l gives several temperatures measured at different power outputs in the piston crowns and piston ring lands of a pressure-oil cooled and a noncooled piston. The comparison clearly shows that although the power output per unit of piston area was considerably increased, the temperatures in the compression ring area, due to the effectiveness of the piston cooling, did not exceed those measured in the conventional standard design. These temperatures determine if seizing of the compression rings will occur. The only temperatures which increased slightly were those in the center of the piston crown. This is due to the considerably higher thermal loading and to a slightly smaller conductivity of the steel crown. Since, however, the crown of the cooled piston is of heat-resistant material and not of aluminum, this temperature rise has no detrimental effect on service life.&lt;br /&gt;
&lt;br /&gt;
So far, in the comparative evaluation of different engines, the common base, namely the engine loading, was understood to refer exclusively to the piston and crankshaft assemblies. However, cylinder heads and liners are both subjected to high stresses. This is due to the explosion pressure and also to the heating of combustion chamber walls during the combustion process.&lt;br /&gt;
&lt;br /&gt;
To simulate the maximum stresses in the cylinder head and liner due to ignition pressure Pz, the tangential stress&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=High-Speed_High-Output_Diesel_Engines&amp;diff=900</id>
		<title>High-Speed High-Output Diesel Engines</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=High-Speed_High-Output_Diesel_Engines&amp;diff=900"/>
		<updated>2026-04-06T18:10:00Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;== High-Speed High-Output Diesel Engines - 35 Years of Development of Railroad and Marine Applications ==&lt;br /&gt;
By Markus von Kienlin and G. W. Maybach &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;History&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
TO THE EXPERT, the name of Maybach Motorenbau immediately recalls a special class of engines characterized by the following outstanding features: high speed, light weight, small size, high fatigue strength (due to special design and production measures,) and low operating cost. &lt;br /&gt;
&lt;br /&gt;
The unique development of the Zeppelin airship after the historic accident at Echterdingen in 1908, was decisively governed by the fact that Wilhelm Maybach, Gottlieb Daimler&#039;s collaborator, made available to Count Zeppelin an engine designed by his son, Karl Maybach. This was a 6-cyl 150 hp 1200 rpm engine with a fuel consumption of 254 g/hph and a weight-to-power ratio of no more than 2,99 kg/hp, in contrast to the engine installed in the first Zeppelin airship which had a weight of 26 kg/hp and a consumption of 508 g/hph. For the production of the new engine, Count Zeppelin and Wilhelm Maybach founded, on March 23, 1909, the Luftfahrzeug-Motorenbau G.m.b.H. which was affilleated to Luftschiffbau Zeppelin. The Maybach Motorenbau, which was entrusted to Karl Maybach from the outset, produced the engines for further Zeppelin airships and for aeroplanes. Among those engines, as early as 1917, highly rated high-compression high-altitude engines were built. Fig. 1 shows such a high-altitude aircraft engine. Fig. 2 is a sectional view of the cylinder liner and wrist pin area.&lt;br /&gt;
&lt;br /&gt;
After the enforced interruption of almost the entire production at the end of World War I, new and related lines of production suitable for the skilled staff had to be found. The choice included Otto and diesel engines for a number of purposes. Research continued on Zeppelin airship engines including the well-known 550 hp VL-type engine (Fig. 3) for the airship &amp;quot;Graf Zeppelin,&amp;quot; which accomplished the famous world tours under the command of the late Dr. Eckener, who until his death in 1954 was chairman of the Maybach Motorenbau. The first powerful high-speed diesel engine was developed in the Maybach workshops between 1919 and 1923. Construction of this G 4 engine (Fig. 4) was a remarkable   venture, bearing in mind that at that time experience with high-speed diesel engines was actually only with submarine engines having a maximum speed of not more than 500 rpm, whereas the new 150 hp Maybach diesel engine had an operating speed of 1300 rpm.&lt;br /&gt;
&lt;br /&gt;
Solid fuel injection was then still at its beginning, so that the G 4 engine had air injection. Fig. 4 shows the relative sizes of the diesel engine and the engine-driven air compressor needed for air injection. &lt;br /&gt;
&lt;br /&gt;
Opinion at that time - which many still hold today - was that the high-speed engines despite their obvious advantages with respect to weight and reduced space requirements would have a shorter service life, have less favorable consumption figures, and be more prone to trouble. This opinion chiefly resulted from the fact that many firms tried to increase the output of their existent low-speed engines merely by increasing the engine speed and neglecting any improvements in design. Naturally, this led to setbacks which in turn gave rise to such widespread opinion. The Maybach Motorenbau, which even then had many years of experience in the field of high-speed Otto engines, adopted new methods by designing a diesel engine especially for high speed and by aiming simultaneously at a corresponding increase of operating reliability and service life, two requirements obviously necessary for airship engines.&lt;br /&gt;
&lt;br /&gt;
Since the first results with high-speed diesel engines were very encouraging, the development of these engines was continued and their output increased. The output of the first 6-cyl engine was soon raised to 210 hp at 1400 rpm. followed in 1930 by a 12-cyl V-engine providing 410 hp at 1400 rpm which, at a later date, was brought to 600 and 650 hp by exhaust gas supercharging (Fig. 5). In 1931 two of these 410 hp GO 5 engines were installed in the &amp;quot;Fliegender Hamburger,&amp;quot; the first high-speed railcar-train of the German State Railway (Fig, 6). Its schedule speed of 77.6 mph, no less than the regular daily top speed of 100 mph, on the route between Hamburg and Berlin was a sensation at the time among railroad experts. &lt;br /&gt;
&lt;br /&gt;
These Maybach engines of the GO-type - primarily designed as power units for railcars - set the fashion for diesel train operation of this power class in Europe until the year 1940. Hundreds of railcars and diesel trains were equipped with these engines in Germany, France, Belgium, Holland, Sweden, Norway, and Spain. Moreover, the engines met with favorable reception in naval construction, and were increasingly used for high-speed passenger boats, customs cruisers, yachts, coastguard crafts, and other craft. &lt;br /&gt;
&lt;br /&gt;
The GO-type were designed so that the cylinder blocks of 6.30 in. bore and 7.88 in. stroke, made in one casting with the cylinder head, were assembled in an aluminum crankcase. The engines had direct injection, and four valves per cylinder controlled by overhead camshafts.&lt;br /&gt;
&lt;br /&gt;
tons were made of aluminum. Convenient mounting of run-&lt;br /&gt;
&lt;br /&gt;
ning parts posed a special problem at the time for these pow-&lt;br /&gt;
&lt;br /&gt;
White metal bearings could not be used, and&lt;br /&gt;
&lt;br /&gt;
lead-bronze bearings were still in too early stages of develop-&lt;br /&gt;
&lt;br /&gt;
ment. Therefore, it was decided to provide both the crank-&lt;br /&gt;
&lt;br /&gt;
shaft and big ends with roller bearings, the composition of&lt;br /&gt;
&lt;br /&gt;
material and thermal treatment for which were the subject&lt;br /&gt;
&lt;br /&gt;
of lengthy and painstaking development by the company.&lt;br /&gt;
&lt;br /&gt;
In operation, these engines attained mileages between&lt;br /&gt;
&lt;br /&gt;
general overhauls of as much as 100,000 miles (about 2500 operating hours) and more, which prior to World War I was&lt;br /&gt;
&lt;br /&gt;
regarded as quite satisfactory.&lt;br /&gt;
&lt;br /&gt;
After termination of World War Il the situation was en-&lt;br /&gt;
&lt;br /&gt;
tirely different. Under the influence of the immense ad-&lt;br /&gt;
&lt;br /&gt;
vance of the diesel locomotive in the United States and else-&lt;br /&gt;
&lt;br /&gt;
where, railway companies became increasingly interested&lt;br /&gt;
&lt;br /&gt;
in converting their heavy traction service to diesel operation.&lt;br /&gt;
&lt;br /&gt;
If European manufacturers wanted to take part in this de-&lt;br /&gt;
&lt;br /&gt;
velopment, they had to counter the American diesel lo-&lt;br /&gt;
&lt;br /&gt;
comotive with its heavy and slow-running engine by a type&lt;br /&gt;
&lt;br /&gt;
of vehicle which would be available for a more universal&lt;br /&gt;
&lt;br /&gt;
application, offer more favorable weight conditions, and&lt;br /&gt;
&lt;br /&gt;
which in respect of output and service life would at least&lt;br /&gt;
&lt;br /&gt;
equal the heavy engines.&lt;br /&gt;
&lt;br /&gt;
For Maybach Motorenbau, as the representative of the&lt;br /&gt;
&lt;br /&gt;
European trend, the demand for long life of the engine and&lt;br /&gt;
&lt;br /&gt;
components became&lt;br /&gt;
&lt;br /&gt;
small-size engines had to be designed which would be cap-&lt;br /&gt;
&lt;br /&gt;
able of offering mileages between overhauls at least equal&lt;br /&gt;
&lt;br /&gt;
to those then attained in rail traction by the finest types of&lt;br /&gt;
&lt;br /&gt;
slow-speed engines. Beyond that, these engines were sup-&lt;br /&gt;
&lt;br /&gt;
posed not only to compete successfully in the field of diesel&lt;br /&gt;
&lt;br /&gt;
traction, but also to conquer new fields of application.&lt;br /&gt;
&lt;br /&gt;
Considering that for the aforementioned GO-type engines&lt;br /&gt;
&lt;br /&gt;
the roller bearings in the big end of the connecting rods were&lt;br /&gt;
&lt;br /&gt;
the limiting factor for the running performance, it was ob-&lt;br /&gt;
&lt;br /&gt;
vious that further development should aim at plain bearings&lt;br /&gt;
&lt;br /&gt;
for the big ends and a modernization of all running parts.&lt;br /&gt;
&lt;br /&gt;
The best solution in this direction appeared to be the disc-&lt;br /&gt;
&lt;br /&gt;
webbed crankshaft, which inherently has greatly improved&lt;br /&gt;
&lt;br /&gt;
vibration characteristics, and which also provides ideal con-&lt;br /&gt;
&lt;br /&gt;
ditions for the entire bearing problem.&lt;br /&gt;
&lt;br /&gt;
This was confirmed by the experience gained by May-&lt;br /&gt;
&lt;br /&gt;
bach Motorenbau during the last war with more than 50,000&lt;br /&gt;
&lt;br /&gt;
Otto engines ranging from 300 to 700 hp at 3000 rpm, equip-&lt;br /&gt;
&lt;br /&gt;
ped with disc-webbed crankshafts and installed in heavy-&lt;br /&gt;
&lt;br /&gt;
duty military vehicles (tanks and heavy trucks).a s a m a t e r&lt;br /&gt;
&lt;br /&gt;
of fact, the adaptation of the disc-webbed crankshaft to the&lt;br /&gt;
&lt;br /&gt;
aforementioned pre-war GO-type, resulted in the change-over to the so-called GTO-&amp;quot;tunnel&amp;quot; type crankcase, repre-&lt;br /&gt;
&lt;br /&gt;
senting a unique jump ahead in development.&lt;br /&gt;
&lt;br /&gt;
Proof of this was the service results achieved by the Ger-&lt;br /&gt;
&lt;br /&gt;
man Federal Railway with its 600 bhp Maybach GTO type&lt;br /&gt;
&lt;br /&gt;
tunnel engines. It was revealed by spot checks that the bear-&lt;br /&gt;
&lt;br /&gt;
ings of these engines operating at 1400 rpm were still like&lt;br /&gt;
&lt;br /&gt;
new after distances of 300,000-400,000 miles. All other&lt;br /&gt;
&lt;br /&gt;
wearing parts showed such slight wear that a general over-&lt;br /&gt;
&lt;br /&gt;
haul was not anticipated before 600,000-700,000 miles, cor-&lt;br /&gt;
&lt;br /&gt;
responding to about 12,000 to 15,000 operating hr. Early&lt;br /&gt;
&lt;br /&gt;
in 1955, these 600 bhp engines had exceeded an aggregate&lt;br /&gt;
&lt;br /&gt;
mileage of more than 6 million miles without any major en-&lt;br /&gt;
&lt;br /&gt;
gine overhauls (1).*&lt;br /&gt;
&lt;br /&gt;
Today there are more than 1000 of these 12-cyl GTO en-&lt;br /&gt;
&lt;br /&gt;
gines rated up to 800 hp in service. Of these 840 are in-&lt;br /&gt;
&lt;br /&gt;
stalled in shunting locomotives of the European standard type&lt;br /&gt;
&lt;br /&gt;
V.60, running for 20,000-25,000 hr before a piston check&lt;br /&gt;
&lt;br /&gt;
is scheduled.&lt;br /&gt;
&lt;br /&gt;
Thus an optimum solution was found for the problems pre-&lt;br /&gt;
&lt;br /&gt;
sented by the running gear of this engine type. For more&lt;br /&gt;
&lt;br /&gt;
powerful engines, however, with continuous outputs of about&lt;br /&gt;
&lt;br /&gt;
100 hp per cylinder and with similar or rather better service&lt;br /&gt;
&lt;br /&gt;
behavior, one more step was necessary. That step was the&lt;br /&gt;
&lt;br /&gt;
introduction of the tunnel construction with roller main bear-&lt;br /&gt;
&lt;br /&gt;
The performance of this&lt;br /&gt;
&lt;br /&gt;
was proved first by thorough trials with powerful diesel en-&lt;br /&gt;
&lt;br /&gt;
gines of a speed range between 2400 and 2600 rpm. Even-&lt;br /&gt;
&lt;br /&gt;
tually this led to the present Maybach MD tunnel engine,&lt;br /&gt;
&lt;br /&gt;
a design which has aroused great interest in the technical&lt;br /&gt;
&lt;br /&gt;
world. With this design, the problem of building a high-&lt;br /&gt;
&lt;br /&gt;
speed diesel engine with a running performance equal to,&lt;br /&gt;
&lt;br /&gt;
of better than that of a good slow-speed engine, can be re-&lt;br /&gt;
&lt;br /&gt;
garded as solved.&lt;br /&gt;
&lt;br /&gt;
Before giving a more detailed description of the MD de-&lt;br /&gt;
&lt;br /&gt;
sign, it may be advantageous to discuss some general prob-&lt;br /&gt;
&lt;br /&gt;
lems pertaining to high engine speed, and to report on the&lt;br /&gt;
&lt;br /&gt;
research techniques which contributed essentially to the de-&lt;br /&gt;
&lt;br /&gt;
velopment of the modern Maybach diesel engines.&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;General Questions Relating to High Engine Speed&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
It is, first of all, necessary to emphasize a fact often&lt;br /&gt;
&lt;br /&gt;
insufficiently realized by users: engine speed alone does not&lt;br /&gt;
&lt;br /&gt;
provide an adequate criterion for the genuine high-speed&lt;br /&gt;
&lt;br /&gt;
character of an engine. Even the mean piston speed does&lt;br /&gt;
&lt;br /&gt;
not provide such a criterion, since the mean effective pres-&lt;br /&gt;
&lt;br /&gt;
sure must also be taken into account, as well as whether the&lt;br /&gt;
&lt;br /&gt;
piston speed is used with high or low mean effective pressure&lt;br /&gt;
&lt;br /&gt;
at equal engine speed.&lt;br /&gt;
&lt;br /&gt;
Some performance characteristics, important as far as&lt;br /&gt;
&lt;br /&gt;
engine loading is concerned, are now considered. Besides&lt;br /&gt;
&lt;br /&gt;
the absolute engine power N and the specific power per cyl-&lt;br /&gt;
&lt;br /&gt;
inder N/z, it is quite common to use the ratio of power per&lt;br /&gt;
&lt;br /&gt;
unit of swept volume N/V, characterizing the degree of util-ization of the swept volume. The ratio of power per unit&lt;br /&gt;
&lt;br /&gt;
of piston area, N/F, also has a bearing in this connection:&lt;br /&gt;
&lt;br /&gt;
it signifies the total engine power related to the total area&lt;br /&gt;
&lt;br /&gt;
of the piston crowns. The piston crown is one of the engine&lt;br /&gt;
&lt;br /&gt;
parts subjected to the highest thermal load. To dissipate&lt;br /&gt;
&lt;br /&gt;
the heat accumulated here by means of conduction, radia-&lt;br /&gt;
&lt;br /&gt;
tion, or coolants is a matter of vital importance which may&lt;br /&gt;
&lt;br /&gt;
well be a limiting factor in increasing the specific engine&lt;br /&gt;
&lt;br /&gt;
power.&lt;br /&gt;
&lt;br /&gt;
Strictly speaking, the ratios of power per unit of displaced&lt;br /&gt;
&lt;br /&gt;
volume, and power per unit of piston area can only pro-&lt;br /&gt;
&lt;br /&gt;
vide a valid scale of comparison if the cylinders compared&lt;br /&gt;
&lt;br /&gt;
have the same size and shape. The influence of the stroke-&lt;br /&gt;
&lt;br /&gt;
to-bore ratio on these parameters has been investigated by&lt;br /&gt;
&lt;br /&gt;
Jaklitsch (2). Under certain limiting assumptions, he found&lt;br /&gt;
&lt;br /&gt;
that this influence is of the order of Vs/d, (s = stroke d =&lt;br /&gt;
&lt;br /&gt;
bore) a result derived statistically for diesel engines designed&lt;br /&gt;
&lt;br /&gt;
for aircraft and road vehicles, and it may be assumed, that&lt;br /&gt;
&lt;br /&gt;
this influence is equally applicable to larger types of diesel&lt;br /&gt;
&lt;br /&gt;
engines.&lt;br /&gt;
&lt;br /&gt;
The fact that the ratio of power per unit of swept vol-&lt;br /&gt;
&lt;br /&gt;
ume is influenced by the stroke-to-bore ratio can be ex-&lt;br /&gt;
&lt;br /&gt;
plained by the fact that as this ratio changes there is also&lt;br /&gt;
&lt;br /&gt;
a change in the ratio of the heat-affected surface to the cor-&lt;br /&gt;
&lt;br /&gt;
responding swept volume. With the longer stroke engine,&lt;br /&gt;
&lt;br /&gt;
where the piston diameter is smaller, the distance of heat&lt;br /&gt;
&lt;br /&gt;
flow from the center of the piston crown to the cylinder wal&lt;br /&gt;
&lt;br /&gt;
is smaller. Therefore, the temperatures at the center of&lt;br /&gt;
&lt;br /&gt;
the piston crown become higher if the piston diameter is&lt;br /&gt;
&lt;br /&gt;
increased. The results of similar investigations on the in-&lt;br /&gt;
&lt;br /&gt;
fluence of cylinder bore and stroke-to-bore ratio on the piston&lt;br /&gt;
&lt;br /&gt;
temperature are plotted in Fig. 7. This graph shows that,&lt;br /&gt;
&lt;br /&gt;
even if mean effective pressure, piston speed, and stroke-&lt;br /&gt;
&lt;br /&gt;
to-bore ratio remain constant, an increase in the cylinder&lt;br /&gt;
&lt;br /&gt;
bore causes higher temperatures at the center of the piston&lt;br /&gt;
&lt;br /&gt;
crown. It will also be noted that the increase is steeper with&lt;br /&gt;
&lt;br /&gt;
short-stroke engines than with long-stroke engines. In order&lt;br /&gt;
&lt;br /&gt;
to obtain more realistic parameters for comparisons, the ratios of power per unit of swept volume and power per unit of piston area must be related to the stroke-to-bore ratio &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Apart from having such parameters as the specific power-to-volume ratio, and the specific power-to-piston area ratio, which are more indicative of the thermal loading of the pistons, it is also of importance to obtain criteria characterizing the mechanical stresses occurring in the rotating crankshaft assembly. This applies in particular to the big-end bearings, the loading of which might be characterized by the mass forces of the rotating and oscillating parts of the engine as well as by the maximum gas pressure. Assuming that, with the application of corresponding design principles, the weights of the rotating and oscillating engine parts vary with the third power of the piston diameter, a parameter a can be formed relating the mass forces to the unit of piston area, for example:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Jaklitsch calls this a value &amp;quot;running index&amp;quot; (2), and as-&lt;br /&gt;
&lt;br /&gt;
cribes to it a major importance. The term &amp;quot;mass-force fac-&lt;br /&gt;
&lt;br /&gt;
tor,&amp;quot; however, appears to be more suitable as it relates more&lt;br /&gt;
&lt;br /&gt;
directly to the significance of the parameter. F o r i t i t 1s&lt;br /&gt;
&lt;br /&gt;
accepted that, with a corresponding utilization of the cyl-&lt;br /&gt;
&lt;br /&gt;
inder diameter, the projected area of the big-end bearings&lt;br /&gt;
&lt;br /&gt;
increases with the square of the piston diameter, the mass-&lt;br /&gt;
&lt;br /&gt;
force factor may well be accepted as a valid criterion for&lt;br /&gt;
&lt;br /&gt;
the bearing load due to the mass forces.&lt;br /&gt;
&lt;br /&gt;
If the two engines compared are geometrically similar,&lt;br /&gt;
&lt;br /&gt;
that is, if the stroke-to-bore ratio remains the same, the&lt;br /&gt;
&lt;br /&gt;
above assumption is strictly true, as the masses in motion&lt;br /&gt;
&lt;br /&gt;
do vary with the third power of the piston diameter. In order&lt;br /&gt;
&lt;br /&gt;
to gain an idea in regard to the variation of the masses act-&lt;br /&gt;
&lt;br /&gt;
ing the big-end b e a r i n g W h e n t e s t o k e - t o - b o r e t a l l o&lt;br /&gt;
&lt;br /&gt;
is modified, this ratio was altered in a V-engine and the&lt;br /&gt;
&lt;br /&gt;
variation of the masses acting on the bearing was calculated.&lt;br /&gt;
&lt;br /&gt;
It was found that when the stroke-to-bore ratio was increased&lt;br /&gt;
&lt;br /&gt;
by as much as 60% the increase in weight was no more&lt;br /&gt;
&lt;br /&gt;
than 2-3%. It follows that, within reasonable limits, the&lt;br /&gt;
&lt;br /&gt;
mistake made by assuming that the variation of masses is&lt;br /&gt;
&lt;br /&gt;
proportional to d3 is insignificant.&lt;br /&gt;
&lt;br /&gt;
F r o m this may be concluded that the engine with the&lt;br /&gt;
&lt;br /&gt;
most efficiently utilized crankshaft is the one which has the&lt;br /&gt;
&lt;br /&gt;
highest mass-force factor a, and, at the same time, can&lt;br /&gt;
&lt;br /&gt;
prove to be reliable in service and to have the service life&lt;br /&gt;
&lt;br /&gt;
expected for its application (5).&lt;br /&gt;
&lt;br /&gt;
The diagram in Fig. 8 is intended to show the signifi-&lt;br /&gt;
&lt;br /&gt;
cance of the mass-force factor. For instance, if an engine has a speed of 1300 rpm and a cylinder bore of 7.28 in.,&lt;br /&gt;
&lt;br /&gt;
with a stroke of 7.78 in. the mass-force factor becomes 672&lt;br /&gt;
&lt;br /&gt;
ft/min?. If the same engine is accelerated to 1800 rpm, the&lt;br /&gt;
&lt;br /&gt;
mass-force factor increases to 1289 ft/min?. With a slow-&lt;br /&gt;
&lt;br /&gt;
speed engine of, say, 250 rpm, 17.72 in. bore and 25.58&lt;br /&gt;
&lt;br /&gt;
in. stroke, the mass-force factor is no greater than 199 ft?/&lt;br /&gt;
&lt;br /&gt;
min?. Since both slow-speed and high-speed engines under&lt;br /&gt;
&lt;br /&gt;
consideration have actually been found to be very reliable&lt;br /&gt;
&lt;br /&gt;
in practice, it follows that the crankshaft assembly of the&lt;br /&gt;
&lt;br /&gt;
high-speed engine is much more efficiently utilized than&lt;br /&gt;
&lt;br /&gt;
that of the slow-speed engine.&lt;br /&gt;
&lt;br /&gt;
In order to explain the significance of the mass-force fac-&lt;br /&gt;
&lt;br /&gt;
tor still more in detail the characteristic parameters have&lt;br /&gt;
&lt;br /&gt;
been determined for some of the most important present-&lt;br /&gt;
&lt;br /&gt;
time locomotive engines of about 1000 bhp and more. The&lt;br /&gt;
&lt;br /&gt;
data are listed in Table 1. Four-cycle engines have been&lt;br /&gt;
&lt;br /&gt;
selected only so as to make a simple comparison of the par-&lt;br /&gt;
&lt;br /&gt;
ameters possible.&lt;br /&gt;
&lt;br /&gt;
Two engines with equal characteristic parameters can&lt;br /&gt;
&lt;br /&gt;
be assumed to show equal service performance of their pis-&lt;br /&gt;
&lt;br /&gt;
ton and crankshaft assemblies. This, however, holds only&lt;br /&gt;
&lt;br /&gt;
for engines of similar design. Therefore the parameters&lt;br /&gt;
&lt;br /&gt;
should never be compared on their own, but only under sim-&lt;br /&gt;
&lt;br /&gt;
ultaneous consideration of the designs of the engines involved.&lt;br /&gt;
&lt;br /&gt;
It appears from Table 1 that the specific power-to-piston&lt;br /&gt;
&lt;br /&gt;
area ratio of the locomotive engines - irrespective of their&lt;br /&gt;
&lt;br /&gt;
power and speed - is within the limits 210 to 345 bhp/ft?,&lt;br /&gt;
&lt;br /&gt;
excluding the engines represented by items 8 and 9, which will be discussed later. For the turbocharged stationary en-&lt;br /&gt;
&lt;br /&gt;
gines, rated at continuous speeds from 250 to 600 rpm, the&lt;br /&gt;
&lt;br /&gt;
respective p o w e r - t o - p i s t o n a r e a r a t i o s r a n g e a p p r o x i m a t e l y&lt;br /&gt;
&lt;br /&gt;
between 93 and 186 bhp/ft?. From this comparison it be-&lt;br /&gt;
&lt;br /&gt;
comes quite evident that the effort to ensure small bulk of&lt;br /&gt;
&lt;br /&gt;
the locomotive engines to make them suitable for their ap-&lt;br /&gt;
&lt;br /&gt;
plication, imposes high demands on engine design as well&lt;br /&gt;
&lt;br /&gt;
as on material when operational reliability and life of the&lt;br /&gt;
&lt;br /&gt;
wearing parts of both engine groups is to be the same. Even&lt;br /&gt;
&lt;br /&gt;
more revealing are here the high mass-force factors for the&lt;br /&gt;
&lt;br /&gt;
locomotive engines which range between 603 and 915 f t /&lt;br /&gt;
&lt;br /&gt;
min&#039;, whereas the corresponding figures for stationary en-&lt;br /&gt;
&lt;br /&gt;
gines lie only between 215 and 431 ft ⅔ /min?.&lt;br /&gt;
&lt;br /&gt;
These simple considerations show that locomotive en-&lt;br /&gt;
&lt;br /&gt;
gines which have proved satisfactory in practical operation&lt;br /&gt;
&lt;br /&gt;
must be types of a highly meritorious design, for they have&lt;br /&gt;
&lt;br /&gt;
withstood the imposition of quite severe demands.&lt;br /&gt;
&lt;br /&gt;
In order to permit a comparison between different en-&lt;br /&gt;
&lt;br /&gt;
gines on the basis of the criteria developed above, a com-&lt;br /&gt;
&lt;br /&gt;
mon basis of &amp;quot;equal loading&amp;quot; has to be defined. &amp;quot;Equal&lt;br /&gt;
&lt;br /&gt;
loading&amp;quot; of two engines specifically means that the mech-&lt;br /&gt;
&lt;br /&gt;
anical and thermal loading of piston and crankshaft assem-&lt;br /&gt;
&lt;br /&gt;
blies of the two engines is the same. This is characterized&lt;br /&gt;
&lt;br /&gt;
by: &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
The conception of geometric similarity is understood to&lt;br /&gt;
&lt;br /&gt;
cover not only the cylinders, (stroke and bore), but also all&lt;br /&gt;
&lt;br /&gt;
those parts of the engine which are subjected to any stresses.&lt;br /&gt;
&lt;br /&gt;
In all these comparisons, the mechanical efficiencies of the&lt;br /&gt;
&lt;br /&gt;
engines are assumed to be constant.&lt;br /&gt;
&lt;br /&gt;
From the well-known engine power equation:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Assuming that for two geometrically similar engines (s/d =&lt;br /&gt;
&lt;br /&gt;
constant) the mean piston speed Cm the mean effective&lt;br /&gt;
&lt;br /&gt;
pressure Po, the swept volume Ve and the ratio N/ are&lt;br /&gt;
&lt;br /&gt;
constant, the correlation between power and number of cyl-&lt;br /&gt;
&lt;br /&gt;
inders becomes:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Fig. 9 shows this functional relationship indicative of the&lt;br /&gt;
&lt;br /&gt;
increase in output obtained with an engine of the same total&lt;br /&gt;
&lt;br /&gt;
swept volume by increasing the number of cylinders.&lt;br /&gt;
&lt;br /&gt;
For instance, if a plant hitherto driven by one slow-speed&lt;br /&gt;
&lt;br /&gt;
12-cyl engine is driven, instead, by eight high-speed 12-&lt;br /&gt;
&lt;br /&gt;
cyl engines which have altogether the same total swept vol-&lt;br /&gt;
&lt;br /&gt;
ume as the one slow-speed engine, the output is doubled&lt;br /&gt;
&lt;br /&gt;
although mechanical and thermal stresses in the piston and&lt;br /&gt;
&lt;br /&gt;
crankshaft assembly are the same. If it were intended to&lt;br /&gt;
&lt;br /&gt;
achieve this doubling of output by enlarging the swept vol-&lt;br /&gt;
&lt;br /&gt;
ume of the single slow-speed engine, the swept volume of&lt;br /&gt;
&lt;br /&gt;
that engine would have to be increased 2.8 times.&lt;br /&gt;
&lt;br /&gt;
Finally, regarding the significance of the parameter of&lt;br /&gt;
&lt;br /&gt;
specific power output per unit of piston area as a factor char-&lt;br /&gt;
&lt;br /&gt;
acterizing engine loading, it may be used to divide engines&lt;br /&gt;
&lt;br /&gt;
into different load or performance categories. For instance&lt;br /&gt;
&lt;br /&gt;
certain ranges of this specific power-to-piston area factor&lt;br /&gt;
&lt;br /&gt;
can be assigned to the category of engines of high specific&lt;br /&gt;
&lt;br /&gt;
output, to the category of vehicle engines, the category of&lt;br /&gt;
&lt;br /&gt;
marine engines, and so on. Under these assumptions can&lt;br /&gt;
&lt;br /&gt;
be derived for N/F/Vs/d = constant and (s/d) = const.: &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
for a given load category and geometrically similar engines,&lt;br /&gt;
&lt;br /&gt;
the specific power-to-swept volume ratio is inversely pro-&lt;br /&gt;
&lt;br /&gt;
portional to the bore.&lt;br /&gt;
&lt;br /&gt;
Fig. 10 shows the relationship between the specific pow-&lt;br /&gt;
&lt;br /&gt;
er-to-swept volume factor and the bore for different values&lt;br /&gt;
&lt;br /&gt;
of the specific power-to-piston area factor. For example,&lt;br /&gt;
&lt;br /&gt;
with geometrically similar engines of equal thermal and mechanical stressing of their piston resp, crankshaft assemblies,&lt;br /&gt;
&lt;br /&gt;
the doubling of the bore would halve the power per unit&lt;br /&gt;
&lt;br /&gt;
swept volume. In the same figure data are plotted for four&lt;br /&gt;
&lt;br /&gt;
high-speed engines belonging to four different performance&lt;br /&gt;
&lt;br /&gt;
categories, and one slow-speed marine propulsion engine.&lt;br /&gt;
&lt;br /&gt;
The data of these engines are listed in Table 2.&lt;br /&gt;
&lt;br /&gt;
Table 2 shows that a normal high-speed engine (for ex-&lt;br /&gt;
&lt;br /&gt;
ample, Engine No. 1) has the same power output per unit&lt;br /&gt;
&lt;br /&gt;
of piston area as the slow-speed marine engine No. 5, where&lt;br /&gt;
&lt;br /&gt;
the power of the latter must be regarded as being rather high&lt;br /&gt;
&lt;br /&gt;
compared with other similar engines. With high-speed en-&lt;br /&gt;
&lt;br /&gt;
gines, however, by means of suitable measures such as pis-&lt;br /&gt;
&lt;br /&gt;
ton cooling the specific power output per unit of piston area&lt;br /&gt;
&lt;br /&gt;
can be increased for marine engines to 304 bhp/ft?, as shown&lt;br /&gt;
&lt;br /&gt;
for No. 3 engine. Yet this still does not exhaust the possi-&lt;br /&gt;
&lt;br /&gt;
bilities of increasing the specific power output. As No. 4&lt;br /&gt;
&lt;br /&gt;
engine shows, by an increase in speed, mean effective pres-&lt;br /&gt;
&lt;br /&gt;
sure, and by other measures, the specific power-to-piston&lt;br /&gt;
&lt;br /&gt;
area factor of the same engine can be raised to beyond 600 bhp/ft?, a value which cannot be approached even remotely&lt;br /&gt;
&lt;br /&gt;
by slow-speed engines. This comparison clearly demonstrates&lt;br /&gt;
&lt;br /&gt;
the possibilities for high-speed engines to increase their spe-&lt;br /&gt;
&lt;br /&gt;
cific power output; it also demonstrates the wide power range&lt;br /&gt;
&lt;br /&gt;
which can be obtained with one and the same engine.&lt;br /&gt;
&lt;br /&gt;
The higher the specific power-to-piston area factor is of an engine which has proved to be reliable in actual service, the higher is the standard of technical development which the particular engine can be said to have reached. Hereby the measures are quite decisive by means of which higher specific power output per unit piston area has been attained, without exerting a detrimental influence on the reliability of the engine.&lt;br /&gt;
&lt;br /&gt;
In the high-speed Maybach MD engines, a great step forward was made with the introduction of pressure-oil piston cooling . Fig. I l gives several temperatures measured at different power outputs in the piston crowns and piston ring lands of a pressure-oil cooled and a noncooled piston. The comparison clearly shows that although the power output per unit of piston area was considerably increased, the temperatures in the compression ring area, due to the effectiveness of the piston cooling, did not exceed those measured in the conventional standard design. These temperatures determine if seizing of the compression rings will occur. The only temperatures which increased slightly were those in the center of the piston crown. This is due to the considerably higher thermal loading and to a slightly smaller conductivity of the steel crown. Since, however, the crown of the cooled piston is of heat-resistant material and not of aluminum, this temperature rise has no detrimental effect on service life.&lt;br /&gt;
&lt;br /&gt;
So far, in the comparative evaluation of different engines, the common base, namely the engine loading, was understood to refer exclusively to the piston and crankshaft assemblies. However, cylinder heads and liners are both subjected to high stresses. This is due to the explosion pressure and also to the heating of combustion chamber walls during the combustion process.&lt;br /&gt;
&lt;br /&gt;
To simulate the maximum stresses in the cylinder head and liner due to ignition pressure Pz, the tangential stress&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=High-Speed_High-Output_Diesel_Engines&amp;diff=899</id>
		<title>High-Speed High-Output Diesel Engines</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=High-Speed_High-Output_Diesel_Engines&amp;diff=899"/>
		<updated>2026-04-06T17:50:48Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: Created page with &amp;quot;== High-Speed High-Output Diesel Engines - 35 Years of Development of Railroad and Marine Applications == By Markus von Kienlin and G. W. Maybach    &amp;#039;&amp;#039;&amp;#039;History&amp;#039;&amp;#039;&amp;#039;  TO THE EXPERT, the name of Maybach Motorenbau immediately recalls a special class of engines characterized by the following outstanding features: high speed, light weight, small size, high fatigue strength (due to special design and production measures,) and low operating cost.   The unique development of the...&amp;quot;&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;== High-Speed High-Output Diesel Engines - 35 Years of Development of Railroad and Marine Applications ==&lt;br /&gt;
By Markus von Kienlin and G. W. Maybach &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;History&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
TO THE EXPERT, the name of Maybach Motorenbau immediately recalls a special class of engines characterized by the following outstanding features: high speed, light weight, small size, high fatigue strength (due to special design and production measures,) and low operating cost. &lt;br /&gt;
&lt;br /&gt;
The unique development of the Zeppelin airship after the historic accident at Echterdingen in 1908, was decisively governed by the fact that Wilhelm Maybach, Gottlieb Daimler&#039;s collaborator, made available to Count Zeppelin an engine designed by his son, Karl Maybach. This was a 6-cyl 150 hp 1200 rpm engine with a fuel consumption of 254 g/hph and a weight-to-power ratio of no more than 2,99 kg/hp, in contrast to the engine installed in the first Zeppelin airship which had a weight of 26 kg/hp and a consumption of 508 g/hph. For the production of the new engine, Count Zeppelin and Wilhelm Maybach founded, on March 23, 1909, the Luftfahrzeug-Motorenbau G.m.b.H. which was affilleated to Luftschiffbau Zeppelin. The Maybach Motorenbau, which was entrusted to Karl Maybach from the outset, produced the engines for further Zeppelin airships and for aeroplanes. Among those engines, as early as 1917, highly rated high-compression high-altitude engines were built. Fig. 1 shows such a high-altitude aircraft engine. Fig. 2 is a sectional view of the cylinder liner and wrist pin area.&lt;br /&gt;
&lt;br /&gt;
After the enforced interruption of almost the entire production at the end of World War I, new and related lines of production suitable for the skilled staff had to be found. The choice included Otto and diesel engines for a number of purposes. Research continued on Zeppelin airship engines including the well-known 550 hp VL-type engine (Fig. 3) for the airship &amp;quot;Graf Zeppelin,&amp;quot; which accomplished the famous world tours under the command of the late Dr. Eckener, who until his death in 1954 was chairman of the Maybach Motorenbau. The first powerful high-speed diesel engine was developed in the Maybach workshops between 1919 and 1923. Construction of this G 4 engine (Fig. 4) was a remarkable   venture, bearing in mind that at that time experience with high-speed diesel engines was actually only with submarine engines having a maximum speed of not more than 500 rpm, whereas the new 150 hp Maybach diesel engine had an operating speed of 1300 rpm.&lt;br /&gt;
&lt;br /&gt;
Solid fuel injection was then still at its beginning, so that the G 4 engine had air injection. Fig. 4 shows the relative sizes of the diesel engine and the engine-driven air compressor needed for air injection. &lt;br /&gt;
&lt;br /&gt;
Opinion at that time - which many still hold today - was that the high-speed engines despite their obvious advantages with respect to weight and reduced space requirements would have a shorter service life, have less favorable consumption figures, and be more prone to trouble. This opinion chiefly resulted from the fact that many firms tried to increase the output of their existent low-speed engines merely by increasing the engine speed and neglecting any improvements in design. Naturally, this led to setbacks which in turn gave rise to such widespread opinion. The Maybach Motorenbau, which even then had many years of experience in the field of high-speed Otto engines, adopted new methods by designing a diesel engine especially for high speed and by aiming simultaneously at a corresponding increase of operating reliability and service life, two requirements obviously necessary for airship engines.&lt;br /&gt;
&lt;br /&gt;
Since the first results with high-speed diesel engines&lt;br /&gt;
&lt;br /&gt;
were very encouraging, the development of these engines was&lt;br /&gt;
&lt;br /&gt;
continued and their output increased. The output of the first&lt;br /&gt;
&lt;br /&gt;
6-cyl engine was soon raised to 210 hp at 1400 rpm.&lt;br /&gt;
&lt;br /&gt;
followed in 1930 by a 12-cyl V-engine providing 410 hp at&lt;br /&gt;
&lt;br /&gt;
1400 rpm which, at a later date, was brought to 600 and 650&lt;br /&gt;
&lt;br /&gt;
hp by exhaust gas supercharging (Fig. 5). In 1931 two of&lt;br /&gt;
&lt;br /&gt;
these 410 hp GO 5 engines were installed in the &amp;quot;Fliegender&lt;br /&gt;
&lt;br /&gt;
Hamburger,&amp;quot; the first high-speed railcar-train of the Ger-&lt;br /&gt;
&lt;br /&gt;
man State Railway (Fig, 6). Its schedule speed of 77.6 mph,&lt;br /&gt;
&lt;br /&gt;
no less than the regular daily top speed of 100 mph, on the&lt;br /&gt;
&lt;br /&gt;
route between Hamburg and Berlin was a sensation at the&lt;br /&gt;
&lt;br /&gt;
time among railroad experts.&lt;br /&gt;
&lt;br /&gt;
These Maybach engines of the GO-type - primarily de-&lt;br /&gt;
&lt;br /&gt;
signed as power units for railcars - set the fashion for diesel&lt;br /&gt;
&lt;br /&gt;
train operation of this power class in Europe until the year&lt;br /&gt;
&lt;br /&gt;
1940. Hundreds of railcars and diesel trains were equipped&lt;br /&gt;
&lt;br /&gt;
with these engines in Germany, France, Belgium, Holland,&lt;br /&gt;
&lt;br /&gt;
Sweden, Norway, and Spain. Moreover, the engines met&lt;br /&gt;
&lt;br /&gt;
with favorable reception in naval construction, and were in-&lt;br /&gt;
&lt;br /&gt;
creasingly used for high-speed passenger boats, customs&lt;br /&gt;
&lt;br /&gt;
cruisers, yachts, coastguard crafts, and other craft.&lt;br /&gt;
&lt;br /&gt;
The GO-type were designed so that the cylinder blocks&lt;br /&gt;
&lt;br /&gt;
of 6.30 in. bore and 7.88 in. stroke, made in one casting&lt;br /&gt;
&lt;br /&gt;
with the cylinder head, were assembled in an aluminum&lt;br /&gt;
&lt;br /&gt;
crankcase. The engines had direct injection, and four valves&lt;br /&gt;
&lt;br /&gt;
per cylinder controlled by overhead camshafts.&lt;br /&gt;
&lt;br /&gt;
tons were made of aluminum. Convenient mounting of run-&lt;br /&gt;
&lt;br /&gt;
ning parts posed a special problem at the time for these pow-&lt;br /&gt;
&lt;br /&gt;
White metal bearings could not be used, and&lt;br /&gt;
&lt;br /&gt;
lead-bronze bearings were still in too early stages of develop-&lt;br /&gt;
&lt;br /&gt;
ment. Therefore, it was decided to provide both the crank-&lt;br /&gt;
&lt;br /&gt;
shaft and big ends with roller bearings, the composition of&lt;br /&gt;
&lt;br /&gt;
material and thermal treatment for which were the subject&lt;br /&gt;
&lt;br /&gt;
of lengthy and painstaking development by the company.&lt;br /&gt;
&lt;br /&gt;
In operation, these engines attained mileages between&lt;br /&gt;
&lt;br /&gt;
general overhauls of as much as 100,000 miles (about 2500 operating hours) and more, which prior to World War I was&lt;br /&gt;
&lt;br /&gt;
regarded as quite satisfactory.&lt;br /&gt;
&lt;br /&gt;
After termination of World War Il the situation was en-&lt;br /&gt;
&lt;br /&gt;
tirely different. Under the influence of the immense ad-&lt;br /&gt;
&lt;br /&gt;
vance of the diesel locomotive in the United States and else-&lt;br /&gt;
&lt;br /&gt;
where, railway companies became increasingly interested&lt;br /&gt;
&lt;br /&gt;
in converting their heavy traction service to diesel operation.&lt;br /&gt;
&lt;br /&gt;
If European manufacturers wanted to take part in this de-&lt;br /&gt;
&lt;br /&gt;
velopment, they had to counter the American diesel lo-&lt;br /&gt;
&lt;br /&gt;
comotive with its heavy and slow-running engine by a type&lt;br /&gt;
&lt;br /&gt;
of vehicle which would be available for a more universal&lt;br /&gt;
&lt;br /&gt;
application, offer more favorable weight conditions, and&lt;br /&gt;
&lt;br /&gt;
which in respect of output and service life would at least&lt;br /&gt;
&lt;br /&gt;
equal the heavy engines.&lt;br /&gt;
&lt;br /&gt;
For Maybach Motorenbau, as the representative of the&lt;br /&gt;
&lt;br /&gt;
European trend, the demand for long life of the engine and&lt;br /&gt;
&lt;br /&gt;
components became&lt;br /&gt;
&lt;br /&gt;
small-size engines had to be designed which would be cap-&lt;br /&gt;
&lt;br /&gt;
able of offering mileages between overhauls at least equal&lt;br /&gt;
&lt;br /&gt;
to those then attained in rail traction by the finest types of&lt;br /&gt;
&lt;br /&gt;
slow-speed engines. Beyond that, these engines were sup-&lt;br /&gt;
&lt;br /&gt;
posed not only to compete successfully in the field of diesel&lt;br /&gt;
&lt;br /&gt;
traction, but also to conquer new fields of application.&lt;br /&gt;
&lt;br /&gt;
Considering that for the aforementioned GO-type engines&lt;br /&gt;
&lt;br /&gt;
the roller bearings in the big end of the connecting rods were&lt;br /&gt;
&lt;br /&gt;
the limiting factor for the running performance, it was ob-&lt;br /&gt;
&lt;br /&gt;
vious that further development should aim at plain bearings&lt;br /&gt;
&lt;br /&gt;
for the big ends and a modernization of all running parts.&lt;br /&gt;
&lt;br /&gt;
The best solution in this direction appeared to be the disc-&lt;br /&gt;
&lt;br /&gt;
webbed crankshaft, which inherently has greatly improved&lt;br /&gt;
&lt;br /&gt;
vibration characteristics, and which also provides ideal con-&lt;br /&gt;
&lt;br /&gt;
ditions for the entire bearing problem.&lt;br /&gt;
&lt;br /&gt;
This was confirmed by the experience gained by May-&lt;br /&gt;
&lt;br /&gt;
bach Motorenbau during the last war with more than 50,000&lt;br /&gt;
&lt;br /&gt;
Otto engines ranging from 300 to 700 hp at 3000 rpm, equip-&lt;br /&gt;
&lt;br /&gt;
ped with disc-webbed crankshafts and installed in heavy-&lt;br /&gt;
&lt;br /&gt;
duty military vehicles (tanks and heavy trucks).a s a m a t e r&lt;br /&gt;
&lt;br /&gt;
of fact, the adaptation of the disc-webbed crankshaft to the&lt;br /&gt;
&lt;br /&gt;
aforementioned pre-war GO-type, resulted in the change-over to the so-called GTO-&amp;quot;tunnel&amp;quot; type crankcase, repre-&lt;br /&gt;
&lt;br /&gt;
senting a unique jump ahead in development.&lt;br /&gt;
&lt;br /&gt;
Proof of this was the service results achieved by the Ger-&lt;br /&gt;
&lt;br /&gt;
man Federal Railway with its 600 bhp Maybach GTO type&lt;br /&gt;
&lt;br /&gt;
tunnel engines. It was revealed by spot checks that the bear-&lt;br /&gt;
&lt;br /&gt;
ings of these engines operating at 1400 rpm were still like&lt;br /&gt;
&lt;br /&gt;
new after distances of 300,000-400,000 miles. All other&lt;br /&gt;
&lt;br /&gt;
wearing parts showed such slight wear that a general over-&lt;br /&gt;
&lt;br /&gt;
haul was not anticipated before 600,000-700,000 miles, cor-&lt;br /&gt;
&lt;br /&gt;
responding to about 12,000 to 15,000 operating hr. Early&lt;br /&gt;
&lt;br /&gt;
in 1955, these 600 bhp engines had exceeded an aggregate&lt;br /&gt;
&lt;br /&gt;
mileage of more than 6 million miles without any major en-&lt;br /&gt;
&lt;br /&gt;
gine overhauls (1).*&lt;br /&gt;
&lt;br /&gt;
Today there are more than 1000 of these 12-cyl GTO en-&lt;br /&gt;
&lt;br /&gt;
gines rated up to 800 hp in service. Of these 840 are in-&lt;br /&gt;
&lt;br /&gt;
stalled in shunting locomotives of the European standard type&lt;br /&gt;
&lt;br /&gt;
V.60, running for 20,000-25,000 hr before a piston check&lt;br /&gt;
&lt;br /&gt;
is scheduled.&lt;br /&gt;
&lt;br /&gt;
Thus an optimum solution was found for the problems pre-&lt;br /&gt;
&lt;br /&gt;
sented by the running gear of this engine type. For more&lt;br /&gt;
&lt;br /&gt;
powerful engines, however, with continuous outputs of about&lt;br /&gt;
&lt;br /&gt;
100 hp per cylinder and with similar or rather better service&lt;br /&gt;
&lt;br /&gt;
behavior, one more step was necessary. That step was the&lt;br /&gt;
&lt;br /&gt;
introduction of the tunnel construction with roller main bear-&lt;br /&gt;
&lt;br /&gt;
The performance of this&lt;br /&gt;
&lt;br /&gt;
was proved first by thorough trials with powerful diesel en-&lt;br /&gt;
&lt;br /&gt;
gines of a speed range between 2400 and 2600 rpm. Even-&lt;br /&gt;
&lt;br /&gt;
tually this led to the present Maybach MD tunnel engine,&lt;br /&gt;
&lt;br /&gt;
a design which has aroused great interest in the technical&lt;br /&gt;
&lt;br /&gt;
world. With this design, the problem of building a high-&lt;br /&gt;
&lt;br /&gt;
speed diesel engine with a running performance equal to,&lt;br /&gt;
&lt;br /&gt;
of better than that of a good slow-speed engine, can be re-&lt;br /&gt;
&lt;br /&gt;
garded as solved.&lt;br /&gt;
&lt;br /&gt;
Before giving a more detailed description of the MD de-&lt;br /&gt;
&lt;br /&gt;
sign, it may be advantageous to discuss some general prob-&lt;br /&gt;
&lt;br /&gt;
lems pertaining to high engine speed, and to report on the&lt;br /&gt;
&lt;br /&gt;
research techniques which contributed essentially to the de-&lt;br /&gt;
&lt;br /&gt;
velopment of the modern Maybach diesel engines.&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;General Questions Relating to High Engine Speed&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
It is, first of all, necessary to emphasize a fact often&lt;br /&gt;
&lt;br /&gt;
insufficiently realized by users: engine speed alone does not&lt;br /&gt;
&lt;br /&gt;
provide an adequate criterion for the genuine high-speed&lt;br /&gt;
&lt;br /&gt;
character of an engine. Even the mean piston speed does&lt;br /&gt;
&lt;br /&gt;
not provide such a criterion, since the mean effective pres-&lt;br /&gt;
&lt;br /&gt;
sure must also be taken into account, as well as whether the&lt;br /&gt;
&lt;br /&gt;
piston speed is used with high or low mean effective pressure&lt;br /&gt;
&lt;br /&gt;
at equal engine speed.&lt;br /&gt;
&lt;br /&gt;
Some performance characteristics, important as far as&lt;br /&gt;
&lt;br /&gt;
engine loading is concerned, are now considered. Besides&lt;br /&gt;
&lt;br /&gt;
the absolute engine power N and the specific power per cyl-&lt;br /&gt;
&lt;br /&gt;
inder N/z, it is quite common to use the ratio of power per&lt;br /&gt;
&lt;br /&gt;
unit of swept volume N/V, characterizing the degree of util-ization of the swept volume. The ratio of power per unit&lt;br /&gt;
&lt;br /&gt;
of piston area, N/F, also has a bearing in this connection:&lt;br /&gt;
&lt;br /&gt;
it signifies the total engine power related to the total area&lt;br /&gt;
&lt;br /&gt;
of the piston crowns. The piston crown is one of the engine&lt;br /&gt;
&lt;br /&gt;
parts subjected to the highest thermal load. To dissipate&lt;br /&gt;
&lt;br /&gt;
the heat accumulated here by means of conduction, radia-&lt;br /&gt;
&lt;br /&gt;
tion, or coolants is a matter of vital importance which may&lt;br /&gt;
&lt;br /&gt;
well be a limiting factor in increasing the specific engine&lt;br /&gt;
&lt;br /&gt;
power.&lt;br /&gt;
&lt;br /&gt;
Strictly speaking, the ratios of power per unit of displaced&lt;br /&gt;
&lt;br /&gt;
volume, and power per unit of piston area can only pro-&lt;br /&gt;
&lt;br /&gt;
vide a valid scale of comparison if the cylinders compared&lt;br /&gt;
&lt;br /&gt;
have the same size and shape. The influence of the stroke-&lt;br /&gt;
&lt;br /&gt;
to-bore ratio on these parameters has been investigated by&lt;br /&gt;
&lt;br /&gt;
Jaklitsch (2). Under certain limiting assumptions, he found&lt;br /&gt;
&lt;br /&gt;
that this influence is of the order of Vs/d, (s = stroke d =&lt;br /&gt;
&lt;br /&gt;
bore) a result derived statistically for diesel engines designed&lt;br /&gt;
&lt;br /&gt;
for aircraft and road vehicles, and it may be assumed, that&lt;br /&gt;
&lt;br /&gt;
this influence is equally applicable to larger types of diesel&lt;br /&gt;
&lt;br /&gt;
engines.&lt;br /&gt;
&lt;br /&gt;
The fact that the ratio of power per unit of swept vol-&lt;br /&gt;
&lt;br /&gt;
ume is influenced by the stroke-to-bore ratio can be ex-&lt;br /&gt;
&lt;br /&gt;
plained by the fact that as this ratio changes there is also&lt;br /&gt;
&lt;br /&gt;
a change in the ratio of the heat-affected surface to the cor-&lt;br /&gt;
&lt;br /&gt;
responding swept volume. With the longer stroke engine,&lt;br /&gt;
&lt;br /&gt;
where the piston diameter is smaller, the distance of heat&lt;br /&gt;
&lt;br /&gt;
flow from the center of the piston crown to the cylinder wal&lt;br /&gt;
&lt;br /&gt;
is smaller. Therefore, the temperatures at the center of&lt;br /&gt;
&lt;br /&gt;
the piston crown become higher if the piston diameter is&lt;br /&gt;
&lt;br /&gt;
increased. The results of similar investigations on the in-&lt;br /&gt;
&lt;br /&gt;
fluence of cylinder bore and stroke-to-bore ratio on the piston&lt;br /&gt;
&lt;br /&gt;
temperature are plotted in Fig. 7. This graph shows that,&lt;br /&gt;
&lt;br /&gt;
even if mean effective pressure, piston speed, and stroke-&lt;br /&gt;
&lt;br /&gt;
to-bore ratio remain constant, an increase in the cylinder&lt;br /&gt;
&lt;br /&gt;
bore causes higher temperatures at the center of the piston&lt;br /&gt;
&lt;br /&gt;
crown. It will also be noted that the increase is steeper with&lt;br /&gt;
&lt;br /&gt;
short-stroke engines than with long-stroke engines. In order&lt;br /&gt;
&lt;br /&gt;
to obtain more realistic parameters for comparisons, the ratios of power per unit of swept volume and power per unit of piston area must be related to the stroke-to-bore ratio &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Apart from having such parameters as the specific power-to-volume ratio, and the specific power-to-piston area ratio, which are more indicative of the thermal loading of the pistons, it is also of importance to obtain criteria characterizing the mechanical stresses occurring in the rotating crankshaft assembly. This applies in particular to the big-end bearings, the loading of which might be characterized by the mass forces of the rotating and oscillating parts of the engine as well as by the maximum gas pressure. Assuming that, with the application of corresponding design principles, the weights of the rotating and oscillating engine parts vary with the third power of the piston diameter, a parameter a can be formed relating the mass forces to the unit of piston area, for example:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Jaklitsch calls this a value &amp;quot;running index&amp;quot; (2), and as-&lt;br /&gt;
&lt;br /&gt;
cribes to it a major importance. The term &amp;quot;mass-force fac-&lt;br /&gt;
&lt;br /&gt;
tor,&amp;quot; however, appears to be more suitable as it relates more&lt;br /&gt;
&lt;br /&gt;
directly to the significance of the parameter. F o r i t i t 1s&lt;br /&gt;
&lt;br /&gt;
accepted that, with a corresponding utilization of the cyl-&lt;br /&gt;
&lt;br /&gt;
inder diameter, the projected area of the big-end bearings&lt;br /&gt;
&lt;br /&gt;
increases with the square of the piston diameter, the mass-&lt;br /&gt;
&lt;br /&gt;
force factor may well be accepted as a valid criterion for&lt;br /&gt;
&lt;br /&gt;
the bearing load due to the mass forces.&lt;br /&gt;
&lt;br /&gt;
If the two engines compared are geometrically similar,&lt;br /&gt;
&lt;br /&gt;
that is, if the stroke-to-bore ratio remains the same, the&lt;br /&gt;
&lt;br /&gt;
above assumption is strictly true, as the masses in motion&lt;br /&gt;
&lt;br /&gt;
do vary with the third power of the piston diameter. In order&lt;br /&gt;
&lt;br /&gt;
to gain an idea in regard to the variation of the masses act-&lt;br /&gt;
&lt;br /&gt;
ing the big-end b e a r i n g W h e n t e s t o k e - t o - b o r e t a l l o&lt;br /&gt;
&lt;br /&gt;
is modified, this ratio was altered in a V-engine and the&lt;br /&gt;
&lt;br /&gt;
variation of the masses acting on the bearing was calculated.&lt;br /&gt;
&lt;br /&gt;
It was found that when the stroke-to-bore ratio was increased&lt;br /&gt;
&lt;br /&gt;
by as much as 60% the increase in weight was no more&lt;br /&gt;
&lt;br /&gt;
than 2-3%. It follows that, within reasonable limits, the&lt;br /&gt;
&lt;br /&gt;
mistake made by assuming that the variation of masses is&lt;br /&gt;
&lt;br /&gt;
proportional to d3 is insignificant.&lt;br /&gt;
&lt;br /&gt;
F r o m this may be concluded that the engine with the&lt;br /&gt;
&lt;br /&gt;
most efficiently utilized crankshaft is the one which has the&lt;br /&gt;
&lt;br /&gt;
highest mass-force factor a, and, at the same time, can&lt;br /&gt;
&lt;br /&gt;
prove to be reliable in service and to have the service life&lt;br /&gt;
&lt;br /&gt;
expected for its application (5).&lt;br /&gt;
&lt;br /&gt;
The diagram in Fig. 8 is intended to show the signifi-&lt;br /&gt;
&lt;br /&gt;
cance of the mass-force factor. For instance, if an engine has a speed of 1300 rpm and a cylinder bore of 7.28 in.,&lt;br /&gt;
&lt;br /&gt;
with a stroke of 7.78 in. the mass-force factor becomes 672&lt;br /&gt;
&lt;br /&gt;
ft/min?. If the same engine is accelerated to 1800 rpm, the&lt;br /&gt;
&lt;br /&gt;
mass-force factor increases to 1289 ft/min?. With a slow-&lt;br /&gt;
&lt;br /&gt;
speed engine of, say, 250 rpm, 17.72 in. bore and 25.58&lt;br /&gt;
&lt;br /&gt;
in. stroke, the mass-force factor is no greater than 199 ft?/&lt;br /&gt;
&lt;br /&gt;
min?. Since both slow-speed and high-speed engines under&lt;br /&gt;
&lt;br /&gt;
consideration have actually been found to be very reliable&lt;br /&gt;
&lt;br /&gt;
in practice, it follows that the crankshaft assembly of the&lt;br /&gt;
&lt;br /&gt;
high-speed engine is much more efficiently utilized than&lt;br /&gt;
&lt;br /&gt;
that of the slow-speed engine.&lt;br /&gt;
&lt;br /&gt;
In order to explain the significance of the mass-force fac-&lt;br /&gt;
&lt;br /&gt;
tor still more in detail the characteristic parameters have&lt;br /&gt;
&lt;br /&gt;
been determined for some of the most important present-&lt;br /&gt;
&lt;br /&gt;
time locomotive engines of about 1000 bhp and more. The&lt;br /&gt;
&lt;br /&gt;
data are listed in Table 1. Four-cycle engines have been&lt;br /&gt;
&lt;br /&gt;
selected only so as to make a simple comparison of the par-&lt;br /&gt;
&lt;br /&gt;
ameters possible.&lt;br /&gt;
&lt;br /&gt;
Two engines with equal characteristic parameters can&lt;br /&gt;
&lt;br /&gt;
be assumed to show equal service performance of their pis-&lt;br /&gt;
&lt;br /&gt;
ton and crankshaft assemblies. This, however, holds only&lt;br /&gt;
&lt;br /&gt;
for engines of similar design. Therefore the parameters&lt;br /&gt;
&lt;br /&gt;
should never be compared on their own, but only under sim-&lt;br /&gt;
&lt;br /&gt;
ultaneous consideration of the designs of the engines involved.&lt;br /&gt;
&lt;br /&gt;
It appears from Table 1 that the specific power-to-piston&lt;br /&gt;
&lt;br /&gt;
area ratio of the locomotive engines - irrespective of their&lt;br /&gt;
&lt;br /&gt;
power and speed - is within the limits 210 to 345 bhp/ft?,&lt;br /&gt;
&lt;br /&gt;
excluding the engines represented by items 8 and 9, which will be discussed later. For the turbocharged stationary en-&lt;br /&gt;
&lt;br /&gt;
gines, rated at continuous speeds from 250 to 600 rpm, the&lt;br /&gt;
&lt;br /&gt;
respective p o w e r - t o - p i s t o n a r e a r a t i o s r a n g e a p p r o x i m a t e l y&lt;br /&gt;
&lt;br /&gt;
between 93 and 186 bhp/ft?. From this comparison it be-&lt;br /&gt;
&lt;br /&gt;
comes quite evident that the effort to ensure small bulk of&lt;br /&gt;
&lt;br /&gt;
the locomotive engines to make them suitable for their ap-&lt;br /&gt;
&lt;br /&gt;
plication, imposes high demands on engine design as well&lt;br /&gt;
&lt;br /&gt;
as on material when operational reliability and life of the&lt;br /&gt;
&lt;br /&gt;
wearing parts of both engine groups is to be the same. Even&lt;br /&gt;
&lt;br /&gt;
more revealing are here the high mass-force factors for the&lt;br /&gt;
&lt;br /&gt;
locomotive engines which range between 603 and 915 f t /&lt;br /&gt;
&lt;br /&gt;
min&#039;, whereas the corresponding figures for stationary en-&lt;br /&gt;
&lt;br /&gt;
gines lie only between 215 and 431 ft ⅔ /min?.&lt;br /&gt;
&lt;br /&gt;
These simple considerations show that locomotive en-&lt;br /&gt;
&lt;br /&gt;
gines which have proved satisfactory in practical operation&lt;br /&gt;
&lt;br /&gt;
must be types of a highly meritorious design, for they have&lt;br /&gt;
&lt;br /&gt;
withstood the imposition of quite severe demands.&lt;br /&gt;
&lt;br /&gt;
In order to permit a comparison between different en-&lt;br /&gt;
&lt;br /&gt;
gines on the basis of the criteria developed above, a com-&lt;br /&gt;
&lt;br /&gt;
mon basis of &amp;quot;equal loading&amp;quot; has to be defined. &amp;quot;Equal&lt;br /&gt;
&lt;br /&gt;
loading&amp;quot; of two engines specifically means that the mech-&lt;br /&gt;
&lt;br /&gt;
anical and thermal loading of piston and crankshaft assem-&lt;br /&gt;
&lt;br /&gt;
blies of the two engines is the same. This is characterized&lt;br /&gt;
&lt;br /&gt;
by: &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
The conception of geometric similarity is understood to&lt;br /&gt;
&lt;br /&gt;
cover not only the cylinders, (stroke and bore), but also all&lt;br /&gt;
&lt;br /&gt;
those parts of the engine which are subjected to any stresses.&lt;br /&gt;
&lt;br /&gt;
In all these comparisons, the mechanical efficiencies of the&lt;br /&gt;
&lt;br /&gt;
engines are assumed to be constant.&lt;br /&gt;
&lt;br /&gt;
From the well-known engine power equation:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Assuming that for two geometrically similar engines (s/d =&lt;br /&gt;
&lt;br /&gt;
constant) the mean piston speed Cm the mean effective&lt;br /&gt;
&lt;br /&gt;
pressure Po, the swept volume Ve and the ratio N/ are&lt;br /&gt;
&lt;br /&gt;
constant, the correlation between power and number of cyl-&lt;br /&gt;
&lt;br /&gt;
inders becomes:&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Fig. 9 shows this functional relationship indicative of the&lt;br /&gt;
&lt;br /&gt;
increase in output obtained with an engine of the same total&lt;br /&gt;
&lt;br /&gt;
swept volume by increasing the number of cylinders.&lt;br /&gt;
&lt;br /&gt;
For instance, if a plant hitherto driven by one slow-speed&lt;br /&gt;
&lt;br /&gt;
12-cyl engine is driven, instead, by eight high-speed 12-&lt;br /&gt;
&lt;br /&gt;
cyl engines which have altogether the same total swept vol-&lt;br /&gt;
&lt;br /&gt;
ume as the one slow-speed engine, the output is doubled&lt;br /&gt;
&lt;br /&gt;
although mechanical and thermal stresses in the piston and&lt;br /&gt;
&lt;br /&gt;
crankshaft assembly are the same. If it were intended to&lt;br /&gt;
&lt;br /&gt;
achieve this doubling of output by enlarging the swept vol-&lt;br /&gt;
&lt;br /&gt;
ume of the single slow-speed engine, the swept volume of&lt;br /&gt;
&lt;br /&gt;
that engine would have to be increased 2.8 times.&lt;br /&gt;
&lt;br /&gt;
Finally, regarding the significance of the parameter of&lt;br /&gt;
&lt;br /&gt;
specific power output per unit of piston area as a factor char-&lt;br /&gt;
&lt;br /&gt;
acterizing engine loading, it may be used to divide engines&lt;br /&gt;
&lt;br /&gt;
into different load or performance categories. For instance&lt;br /&gt;
&lt;br /&gt;
certain ranges of this specific power-to-piston area factor&lt;br /&gt;
&lt;br /&gt;
can be assigned to the category of engines of high specific&lt;br /&gt;
&lt;br /&gt;
output, to the category of vehicle engines, the category of&lt;br /&gt;
&lt;br /&gt;
marine engines, and so on. Under these assumptions can&lt;br /&gt;
&lt;br /&gt;
be derived for N/F/Vs/d = constant and (s/d) = const.: &lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
for a given load category and geometrically similar engines,&lt;br /&gt;
&lt;br /&gt;
the specific power-to-swept volume ratio is inversely pro-&lt;br /&gt;
&lt;br /&gt;
portional to the bore.&lt;br /&gt;
&lt;br /&gt;
Fig. 10 shows the relationship between the specific pow-&lt;br /&gt;
&lt;br /&gt;
er-to-swept volume factor and the bore for different values&lt;br /&gt;
&lt;br /&gt;
of the specific power-to-piston area factor. For example,&lt;br /&gt;
&lt;br /&gt;
with geometrically similar engines of equal thermal and mechanical stressing of their piston resp, crankshaft assemblies,&lt;br /&gt;
&lt;br /&gt;
the doubling of the bore would halve the power per unit&lt;br /&gt;
&lt;br /&gt;
swept volume. In the same figure data are plotted for four&lt;br /&gt;
&lt;br /&gt;
high-speed engines belonging to four different performance&lt;br /&gt;
&lt;br /&gt;
categories, and one slow-speed marine propulsion engine.&lt;br /&gt;
&lt;br /&gt;
The data of these engines are listed in Table 2.&lt;br /&gt;
&lt;br /&gt;
Table 2 shows that a normal high-speed engine (for ex-&lt;br /&gt;
&lt;br /&gt;
ample, Engine No. 1) has the same power output per unit&lt;br /&gt;
&lt;br /&gt;
of piston area as the slow-speed marine engine No. 5, where&lt;br /&gt;
&lt;br /&gt;
the power of the latter must be regarded as being rather high&lt;br /&gt;
&lt;br /&gt;
compared with other similar engines. With high-speed en-&lt;br /&gt;
&lt;br /&gt;
gines, however, by means of suitable measures such as pis-&lt;br /&gt;
&lt;br /&gt;
ton cooling the specific power output per unit of piston area&lt;br /&gt;
&lt;br /&gt;
can be increased for marine engines to 304 bhp/ft?, as shown&lt;br /&gt;
&lt;br /&gt;
for No. 3 engine. Yet this still does not exhaust the possi-&lt;br /&gt;
&lt;br /&gt;
bilities of increasing the specific power output. As No. 4&lt;br /&gt;
&lt;br /&gt;
engine shows, by an increase in speed, mean effective pres-&lt;br /&gt;
&lt;br /&gt;
sure, and by other measures, the specific power-to-piston&lt;br /&gt;
&lt;br /&gt;
area factor of the same engine can be raised to beyond 600 bhp/ft?, a value which cannot be approached even remotely&lt;br /&gt;
&lt;br /&gt;
by slow-speed engines. This comparison clearly demonstrates&lt;br /&gt;
&lt;br /&gt;
the possibilities for high-speed engines to increase their spe-&lt;br /&gt;
&lt;br /&gt;
cific power output; it also demonstrates the wide power range&lt;br /&gt;
&lt;br /&gt;
which can be obtained with one and the same engine.&lt;br /&gt;
&lt;br /&gt;
The higher the specific power-to-piston area factor is of an engine which has proved to be reliable in actual service, the higher is the standard of technical development which the particular engine can be said to have reached. Hereby the measures are quite decisive by means of which higher specific power output per unit piston area has been attained, without exerting a detrimental influence on the reliability of the engine.&lt;br /&gt;
&lt;br /&gt;
In the high-speed Maybach MD engines, a great step forward was made with the introduction of pressure-oil piston cooling . Fig. I l gives several temperatures measured at different power outputs in the piston crowns and piston ring lands of a pressure-oil cooled and a noncooled piston. The comparison clearly shows that although the power output per unit of piston area was considerably increased, the temperatures in the compression ring area, due to the effectiveness of the piston cooling, did not exceed those measured in the conventional standard design. These temperatures determine if seizing of the compression rings will occur. The only temperatures which increased slightly were those in the center of the piston crown. This is due to the considerably higher thermal loading and to a slightly smaller conductivity of the steel crown. Since, however, the crown of the cooled piston is of heat-resistant material and not of aluminum, this temperature rise has no detrimental effect on service life.&lt;br /&gt;
&lt;br /&gt;
So far, in the comparative evaluation of different engines, the common base, namely the engine loading, was understood to refer exclusively to the piston and crankshaft assemblies. However, cylinder heads and liners are both subjected to high stresses. This is due to the explosion pressure and also to the heating of combustion chamber walls during the combustion process.&lt;br /&gt;
&lt;br /&gt;
To simulate the maximum stresses in the cylinder head and liner due to ignition pressure Pz, the tangential stress&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<updated>2026-04-01T18:21:37Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;/* CSS placed here will be applied to all skins */&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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	<entry>
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		<summary type="html">&lt;p&gt;Toro Andersen: Created page with &amp;quot;/* CSS placed here will be applied to all skins */ &amp;lt;!-- Google tag (gtag.js) --&amp;gt; &amp;lt;script async src=&amp;quot;https://www.googletagmanager.com/gtag/js?id=G-9FVP0257LH&amp;quot;&amp;gt;&amp;lt;/script&amp;gt; &amp;lt;script&amp;gt;   window.dataLayer = window.dataLayer || [];   function gtag(){dataLayer.push(arguments);}   gtag(&amp;#039;js&amp;#039;, new Date());    gtag(&amp;#039;config&amp;#039;, &amp;#039;G-9FVP0257LH&amp;#039;); &amp;lt;/script&amp;gt;&amp;quot;&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;/* CSS placed here will be applied to all skins */&lt;br /&gt;
&amp;lt;!-- Google tag (gtag.js) --&amp;gt;&lt;br /&gt;
&amp;lt;script async src=&amp;quot;https://www.googletagmanager.com/gtag/js?id=G-9FVP0257LH&amp;quot;&amp;gt;&amp;lt;/script&amp;gt;&lt;br /&gt;
&amp;lt;script&amp;gt;&lt;br /&gt;
  window.dataLayer = window.dataLayer || [];&lt;br /&gt;
  function gtag(){dataLayer.push(arguments);}&lt;br /&gt;
  gtag(&#039;js&#039;, new Date());&lt;br /&gt;
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		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1950&amp;diff=896</id>
		<title>Engineering Abstracts 1950</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1950&amp;diff=896"/>
		<updated>2026-03-30T14:59:58Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1950 =&lt;br /&gt;
&lt;br /&gt;
== Explosion of Empty Diesel-oil Fuel Tank ==&lt;br /&gt;
The vapours of petrol, when mixed with the proper proportion of air, are highly explosive, a fact which is known to most men whose work requires them to handle this fuel. In some quarters, however, there seems to be an impression that the vapours of Diesel oil are not dangerous. This is a fallacy which , in one recent casualty , caused the death of a workman who was attempting to weld a leak in a Diesel-oil tank . As regards the explosiv equalities of Diesel-oil vapours, these are of approximately the same order as those of petrol. &lt;br /&gt;
&lt;br /&gt;
The reason that Diesel oil is safer to handle than petrol is that it is not as volatile. Consequently the liquid does not evaporate ai readily, and , therefore, at any given temperature, petrol will evolve a greater quantity of fumes than Diesel oil. &lt;br /&gt;
&lt;br /&gt;
When, however, due to heat or other circumstances, Diesel oil has evaporated, its vapours are as dangerous as those of petrol and have only to be mixed  with the correct proportion of air to form a combination merely a waiting a source of ignition to explode. In the case referred to, an un inspected fishing vessel, powered with Dieselmotors, developed a leak in one of its fuel tanks. &lt;br /&gt;
&lt;br /&gt;
A welder was sent for to repair the leak. As preparation for his operations, the tank was emptied of all fuel, but no attempt was made to gas-free it. The welder, who was equiped   with a petrol torch for welding the tank, seated him self on a stool at the end of the tank and prepared to weld the defective seam. &lt;br /&gt;
&lt;br /&gt;
Shortly after the work was begun an explosion occurred which knocked a nearby crew member down without injuring him to any extent and threw the welder against a column in the vessel, fracturing his skull. &lt;br /&gt;
&lt;br /&gt;
A fire ensured and due to the heat, gas, and  smoke, the compartment containing the tanks could not be entered until the arrival of  the town fire department approximately 10 or 15 minutes later, at which time firemen with gas masks extricated the welder from the tank room, placed him in an ambulance, and rushed him to the local hospital where he died approximately 10 hours later. The lesson from this casualty is obvious— no tank which has contained oil fuel, even Bunker C , should be worked on with a welding torch until it has been gas-freed .&lt;br /&gt;
&lt;br /&gt;
— Marine Engineering and Shipping Review, Vol. 55, September 1950, p. 80.&lt;br /&gt;
&lt;br /&gt;
== Diesel Engine Research ==&lt;br /&gt;
This paper reviews Diesel engine research carried out at the Diesel Research Laboratory of Caterpillar Tractor Co. under the sponsorship of the author as Director of Research. For many years intensive effort has been made to understand the combustion process in this type of engine by a better knowledge of the fundamentals of ignition and the mechanism of the combustion process, and this study has been developed in the laboratory on a competitive basis. Originally six combustion  systems were put to trial and a modified precombustion-chamber engine  won the palm of victory on the basis o f its ability to maintain uniformity over extended periods of operation. &lt;br /&gt;
&lt;br /&gt;
Briefly, the character of the comparative combustion studies followed two general classifications: (1) visual comb ustion studies; (2) study of combustion-chamber deposits. In order to make extended studies of  the combustion phenomena by visual means, a quartz window was designed to achieve maximum cleanliness without the distraction of soot condensation on the cold windows. &lt;br /&gt;
&lt;br /&gt;
The author describes the precombustion-chamber process, and deals with the composition of combustion gases, flame duration , temperature distribution, the mechanism of ignition, and comb ustion-chamber deposits. He also discusses the development of fuel-injection equipment, pretiming, precalibrating , and the evolution of the fuel pump; he describes the characteristics of several types of check valve and fuel valve, and the fuel-pump control of engine torque characteristics. Spray  characteristics and the flow through the fuel-valve orifice are also examined. &lt;br /&gt;
&lt;br /&gt;
Comments are made upon materials for cylinder liners and piston rings, and the effect of fuel in clusionson cylinder wear; lubrication is also considered. It is believed that excellent performance has been achieved in the precombustion-chamber engine with aminimum of complication in the fuel-injection equipment, and that the development of this principle of combustion has not yet reached its limit of progress.&lt;br /&gt;
&lt;br /&gt;
— James Clayton Lecture by C. G. A. Rosen, read at a meeting of The Institution of Mechanical Engineers, 14th November 1950.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1950&amp;diff=895</id>
		<title>Engineering Abstracts 1950</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1950&amp;diff=895"/>
		<updated>2026-03-30T07:21:17Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1950 =&lt;br /&gt;
&lt;br /&gt;
== Explosion of Empty Diesel-oil Fuel Tank ==&lt;br /&gt;
The vapours of petrol, when mixed with the proper proportion of air, are highly explosive, a fact which is known to most men whose work requires them to handle this fuel. In some quarters, however, there seems to be an impression that the vapours of Diesel oil are not dangerous. This is a fallacy which , in one recen t casu a lty , cau sed th e d eath o f a w o rk m a n&lt;br /&gt;
&lt;br /&gt;
w h o w a s atte m p tin g to w eld a leak in a Diesel-oil tank . As regards the explosiv equalities of Diesel-oil vapours, these are of approximately the same order as those o f p etrol. T h e reason&lt;br /&gt;
&lt;br /&gt;
th at D iesel o il is safer to h an d le th a n p etro l is th a t it is n o t as vo latile. C o n se q u e n tly th e liq u id does n o t evap o rate ai read ily, an d , th erefo re, at a n y g iv e n tem p eratu re, p e tro l w ill&lt;br /&gt;
&lt;br /&gt;
evo lve a greater q u a n tity o f fu m es th a n D iese l oil. W h e n , h ow ever, d u e to heat o r o th er circu m stan ces, D iese l o il has evap o rated , its v ap o u rs are as d an gero u s as th o se o f p etro l an d&lt;br /&gt;
&lt;br /&gt;
h ave o n ly to be m ix ed w ith th e co rre ct p ro p o rtio n o f air to fo rm a co m b in atio n m erely a w a itin g a sou rce o f ig n itio n to exp lod e. In th e case referred to , an u n in sp ected fish in g vessel,&lt;br /&gt;
&lt;br /&gt;
p ow ered w ith D iese l m o to rs, d evelop ed a leak in on e o f its fu el tan ks. A w eld er w a s sen t fo r to rep air th e leak. A s p rep ara tio n fo r h is o p eratio n s, th e tan k w as em p tied o f all fu el,&lt;br /&gt;
&lt;br /&gt;
b u t n o atte m p t w as m ad e to g as-free it. T h e w eld er, w h o w as eq u ip p ed w ith a p etro l to rc h fo r w e ld in g th e tan k , seated h im self o n a sto ol at th e en d o f th e ta n k an d p rep ared to w eld th e&lt;br /&gt;
&lt;br /&gt;
d efective seam . S h o rtly after th e w o rk w a s b eg u n an ex p lo sio n o ccu rred w h ic h k n o ck ed a n earb y crew m em b er d o w n w ith o u t&lt;br /&gt;
&lt;br /&gt;
in ju rin g h im to a n y exten t an d th re w th e w eld er ag a in st a co lu m n in th e vessel, fra c tu rin g h is sk u ll A fire en su red an d d u e to th e h eat, gas, an d sm oke, th e co m p artm e n t co n ta in in g&lt;br /&gt;
&lt;br /&gt;
th e tan k s co u ld n o t be en tered u n til th e a rriva l o f th e to w n fire d ep artm en t ap p ro x im a tely 10 o r 15 m in u te s later, at w h ic h tim e firem en w ith gas m asks ex tricate d th e w eld er fro m th e&lt;br /&gt;
&lt;br /&gt;
tan k ro o m , p la ced h im in an am b u lan ce, a n d ru sh ed h im to th e lo cal h o sp ital w h ere he d ied a p p ro x im a te ly 10 h o u rs later. The lesson from this ca su a lty is o b v io u s— n o ta n k w h ich has co n ta in ed o il fu el, even B u n k e r C , sh o u ld be w o rk e d o n w ith a w e ld in g to rch u n til it has been gas-freed .&lt;br /&gt;
&lt;br /&gt;
— Marine Engineering and Shipping Review, Vol. 55, September 1950, p. 80.&lt;br /&gt;
&lt;br /&gt;
== Diesel Engine Research ==&lt;br /&gt;
T h is p ap er review s D iesel en g in e research carried o u t at the Diesel Research Laboratory of Caterpillar Tractor Co. under the sponsorship of the author as Director of Research. For many years intensive effort has been made to understand the combustion process in this type of engine by a better knowled g e o f th e fu n d a m en ta ls o f ig n itio n a n d th e m ech an ism o f&lt;br /&gt;
&lt;br /&gt;
th e co m b u stio n p rocess, an d th is stu d y has been d evelop ed&lt;br /&gt;
&lt;br /&gt;
in th e la b o ra to ry o n a co m p etitive basis. O rig in a lly six co m b&lt;br /&gt;
&lt;br /&gt;
u stio n system s w ere p u t to trial an d a m o d ified p reco m b u stio n -&lt;br /&gt;
&lt;br /&gt;
ch am b er en g in e w o n th e p alm o f v ic to ry o n th e basis o f its&lt;br /&gt;
&lt;br /&gt;
a b ility to m ain tain u n ifo rm ity over exten d ed p erio d s o f op eratio&lt;br /&gt;
&lt;br /&gt;
n . B rie fly , th e ch ara cter o f th e co m p ara tiv e co m b u stio n&lt;br /&gt;
&lt;br /&gt;
stu d ies fo llo w e d tw o gen eral cla ssifica tio n s: (1) visu al co m b u stio&lt;br /&gt;
&lt;br /&gt;
n stu d ies; (2) stu d y o f co m b u stio n -ch a m b er d ep osits. In&lt;br /&gt;
&lt;br /&gt;
o rd er to m ake exten d ed stu d ies o f th e co m b u stio n p h en om en a&lt;br /&gt;
&lt;br /&gt;
b y visu al m ean s, a q u a rtz w in d o w w as d esign ed to ach ieve&lt;br /&gt;
&lt;br /&gt;
m ax im u m clean lin ess w ith o u t th e d istractio n o f soot co n d e n satio&lt;br /&gt;
&lt;br /&gt;
n o n th e co ld w in d o w s. T h e a u th o r d escribes th e p reco m b&lt;br /&gt;
&lt;br /&gt;
u stio n -ch am b er p rocess, an d deals w ith th e co m p o sitio n o f&lt;br /&gt;
&lt;br /&gt;
co m b u stio n gases, flam e d u ra tio n , tem p eratu re d istrib u tio n , th e&lt;br /&gt;
&lt;br /&gt;
m ech an ism o f ig n itio n , an d co m b u stio n -ch a m b er dep osits. H e&lt;br /&gt;
&lt;br /&gt;
also d iscu sses th e d evelo p m en t o f fu e l-in je ctio n eq u ip m en t, p retim&lt;br /&gt;
&lt;br /&gt;
in g , p recalib ratin g , an d th e ev o lu tio n o f th e fu el p u m p ; he describes th e ch aracteristics o f several typ es o f ch eck v alve an d&lt;br /&gt;
&lt;br /&gt;
fu el valve, an d th e fu e l-p u m p co n tro l o f en g in e torq u e&lt;br /&gt;
&lt;br /&gt;
ch aracteristics. S p ra y ch aracteristics an d th e flo w th ro u g h the&lt;br /&gt;
&lt;br /&gt;
fu el-va lv e orifice are also exam in ed . C o m m en ts are m ad e u p o n&lt;br /&gt;
&lt;br /&gt;
m aterials fo r cy lin d e r lin ers an d p isto n rin g s, an d th e effect&lt;br /&gt;
&lt;br /&gt;
o f fu el in clu sio n s o n cy lin d e r w ear; lu b ricatio n is also c o n sidered&lt;br /&gt;
&lt;br /&gt;
. It is b elieved th at excellen t p erfo rm a n ce has been&lt;br /&gt;
&lt;br /&gt;
ach ieved in th e p reco m b u stio n -ch a m b er en gin e w ith a m in im u m&lt;br /&gt;
&lt;br /&gt;
o f co m p licatio n in th e fu e l-in je ctio n eq u ip m en t, an d th at th e  d evelopment of this principle o f co m b u stio n h as n o t yet reached its limit of progress.&lt;br /&gt;
&lt;br /&gt;
— James Clayton Lecture by C. G. A. Rosen, read at a meeting of The Institution of Mechanical Engineers, 14th November 1950.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1950&amp;diff=894</id>
		<title>Engineering Abstracts 1950</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1950&amp;diff=894"/>
		<updated>2026-03-29T15:52:31Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1950 =&lt;br /&gt;
&lt;br /&gt;
== Explosion of Empty Diesel-oil Fuel Tank ==&lt;br /&gt;
The vapours of petrol, wh en mixed with the proper proportion of air, are highly explosive, a fact which is known to most m en whose work requires them to handle this fuel. In som e&lt;br /&gt;
&lt;br /&gt;
q u arters, h o w ever, th ere seem s to be an im p ressio n th at the vap o u rs o f D iese l o il are n o t d an gerou s. T h is is a fa lla cy w h ich , in o n e recen t casu a lty , cau sed th e d eath o f a w o rk m a n&lt;br /&gt;
&lt;br /&gt;
w h o w a s atte m p tin g to w eld a leak in a D ie se l-o il tan k . A s regard s th e ex p lo siv e q u alities o f D iese l-o il v a p o u rs, th ese are o f ap p ro x im a tely th e sam e o rd er as th o se o f p etrol. T h e reason&lt;br /&gt;
&lt;br /&gt;
th at D iesel o il is safer to h an d le th a n p etro l is th a t it is n o t as vo latile. C o n se q u e n tly th e liq u id does n o t evap o rate ai read ily, an d , th erefo re, at a n y g iv e n tem p eratu re, p e tro l w ill&lt;br /&gt;
&lt;br /&gt;
evo lve a greater q u a n tity o f fu m es th a n D iese l oil. W h e n , h ow ever, d u e to heat o r o th er circu m stan ces, D iese l o il has evap o rated , its v ap o u rs are as d an gero u s as th o se o f p etro l an d&lt;br /&gt;
&lt;br /&gt;
h ave o n ly to be m ix ed w ith th e co rre ct p ro p o rtio n o f air to fo rm a co m b in atio n m erely a w a itin g a sou rce o f ig n itio n to exp lod e. In th e case referred to , an u n in sp ected fish in g vessel,&lt;br /&gt;
&lt;br /&gt;
p ow ered w ith D iese l m o to rs, d evelop ed a leak in on e o f its fu el tan ks. A w eld er w a s sen t fo r to rep air th e leak. A s p rep ara tio n fo r h is o p eratio n s, th e tan k w as em p tied o f all fu el,&lt;br /&gt;
&lt;br /&gt;
b u t n o atte m p t w as m ad e to g as-free it. T h e w eld er, w h o w as eq u ip p ed w ith a p etro l to rc h fo r w e ld in g th e tan k , seated h im self o n a sto ol at th e en d o f th e ta n k an d p rep ared to w eld th e&lt;br /&gt;
&lt;br /&gt;
d efective seam . S h o rtly after th e w o rk w a s b eg u n an ex p lo sio n o ccu rred w h ic h k n o ck ed a n earb y crew m em b er d o w n w ith o u t&lt;br /&gt;
&lt;br /&gt;
in ju rin g h im to a n y exten t an d th re w th e w eld er ag a in st a co lu m n in th e vessel, fra c tu rin g h is sk u ll A fire en su red an d d u e to th e h eat, gas, an d sm oke, th e co m p artm e n t co n ta in in g&lt;br /&gt;
&lt;br /&gt;
th e tan k s co u ld n o t be en tered u n til th e a rriva l o f th e to w n fire d ep artm en t ap p ro x im a tely 10 o r 15 m in u te s later, at w h ic h tim e firem en w ith gas m asks ex tricate d th e w eld er fro m th e&lt;br /&gt;
&lt;br /&gt;
tan k ro o m , p la ced h im in an am b u lan ce, a n d ru sh ed h im to th e lo cal h o sp ital w h ere he d ied a p p ro x im a te ly 10 h o u rs later. The lesson from this ca su a lty is o b v io u s— n o ta n k w h ich has co n ta in ed o il fu el, even B u n k e r C , sh o u ld be w o rk e d o n w ith a w e ld in g to rch u n til it has been gas-freed .&lt;br /&gt;
&lt;br /&gt;
— Marine Engineering and Shipping Review, Vol. 55, September 1950, p. 80.&lt;br /&gt;
&lt;br /&gt;
== Diesel Engine Research ==&lt;br /&gt;
T h is p ap er review s D iesel en g in e research carried o u t at the Diesel Research Laboratory of Caterpillar Tractor Co. under the sponsorship of the author as Director of Research. For many years intensive effort has been made to understand the combustion process in this type of engine by a better knowled g e o f th e fu n d a m en ta ls o f ig n itio n a n d th e m ech an ism o f&lt;br /&gt;
&lt;br /&gt;
th e co m b u stio n p rocess, an d th is stu d y has been d evelop ed&lt;br /&gt;
&lt;br /&gt;
in th e la b o ra to ry o n a co m p etitive basis. O rig in a lly six co m b&lt;br /&gt;
&lt;br /&gt;
u stio n system s w ere p u t to trial an d a m o d ified p reco m b u stio n -&lt;br /&gt;
&lt;br /&gt;
ch am b er en g in e w o n th e p alm o f v ic to ry o n th e basis o f its&lt;br /&gt;
&lt;br /&gt;
a b ility to m ain tain u n ifo rm ity over exten d ed p erio d s o f op eratio&lt;br /&gt;
&lt;br /&gt;
n . B rie fly , th e ch ara cter o f th e co m p ara tiv e co m b u stio n&lt;br /&gt;
&lt;br /&gt;
stu d ies fo llo w e d tw o gen eral cla ssifica tio n s: (1) visu al co m b u stio&lt;br /&gt;
&lt;br /&gt;
n stu d ies; (2) stu d y o f co m b u stio n -ch a m b er d ep osits. In&lt;br /&gt;
&lt;br /&gt;
o rd er to m ake exten d ed stu d ies o f th e co m b u stio n p h en om en a&lt;br /&gt;
&lt;br /&gt;
b y visu al m ean s, a q u a rtz w in d o w w as d esign ed to ach ieve&lt;br /&gt;
&lt;br /&gt;
m ax im u m clean lin ess w ith o u t th e d istractio n o f soot co n d e n satio&lt;br /&gt;
&lt;br /&gt;
n o n th e co ld w in d o w s. T h e a u th o r d escribes th e p reco m b&lt;br /&gt;
&lt;br /&gt;
u stio n -ch am b er p rocess, an d deals w ith th e co m p o sitio n o f&lt;br /&gt;
&lt;br /&gt;
co m b u stio n gases, flam e d u ra tio n , tem p eratu re d istrib u tio n , th e&lt;br /&gt;
&lt;br /&gt;
m ech an ism o f ig n itio n , an d co m b u stio n -ch a m b er dep osits. H e&lt;br /&gt;
&lt;br /&gt;
also d iscu sses th e d evelo p m en t o f fu e l-in je ctio n eq u ip m en t, p retim&lt;br /&gt;
&lt;br /&gt;
in g , p recalib ratin g , an d th e ev o lu tio n o f th e fu el p u m p ; he describes th e ch aracteristics o f several typ es o f ch eck v alve an d&lt;br /&gt;
&lt;br /&gt;
fu el valve, an d th e fu e l-p u m p co n tro l o f en g in e torq u e&lt;br /&gt;
&lt;br /&gt;
ch aracteristics. S p ra y ch aracteristics an d th e flo w th ro u g h the&lt;br /&gt;
&lt;br /&gt;
fu el-va lv e orifice are also exam in ed . C o m m en ts are m ad e u p o n&lt;br /&gt;
&lt;br /&gt;
m aterials fo r cy lin d e r lin ers an d p isto n rin g s, an d th e effect&lt;br /&gt;
&lt;br /&gt;
o f fu el in clu sio n s o n cy lin d e r w ear; lu b ricatio n is also c o n sidered&lt;br /&gt;
&lt;br /&gt;
. It is b elieved th at excellen t p erfo rm a n ce has been&lt;br /&gt;
&lt;br /&gt;
ach ieved in th e p reco m b u stio n -ch a m b er en gin e w ith a m in im u m&lt;br /&gt;
&lt;br /&gt;
o f co m p licatio n in th e fu e l-in je ctio n eq u ip m en t, an d th at th e  d evelopment of this principle o f co m b u stio n h as n o t yet reached its limit of progress.&lt;br /&gt;
&lt;br /&gt;
— James Clayton Lecture by C. G. A. Rosen, read at a meeting of The Institution of Mechanical Engineers, 14th November 1950.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1949&amp;diff=893</id>
		<title>Engineering Abstracts 1949</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1949&amp;diff=893"/>
		<updated>2026-03-28T20:38:42Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1949 =&lt;br /&gt;
&lt;br /&gt;
== Modern Trends in the Development of High-Powered Diesel Machinery ==&lt;br /&gt;
CARSTENSEN, H. &#039;&#039;Trans. Institute of Naval Architects, paper read&#039;&#039; 2 Sept. 1949.&lt;br /&gt;
&lt;br /&gt;
Typical examples are given of high-powered marine Diesel plants of more than 16,000 b.h.p. built between 1926 and 1939. Of these, the double-acting four-stroke engine has been abandoned, and the single-acting four-stroke engine is now used very little for larger ships, though it may be preferred under particularly difficult service conditions because of its simple and robust design, moreover, tests with high-pressure supercharge have shown that its output can be increased considerably. The remaining engine types mentioned are two-stroke engines, single-acting or double-acting, having either loop scavenging or uniflow scavenging. These two-stroke engine types and the four-stroke single-acting engine have been developed into fast-running units whereby any output desired can be furnished by geared or Diesel-electric plants.&lt;br /&gt;
&lt;br /&gt;
In passenger ships the arrangement of the accommodation will determine whether steam-turbine plants, fast-running Diesel engines with geared or electric transmission, or slow-running Diesel engines coupled directly to the propeller shafts will be most advantageous. The Diesel plants, particularly the direct-coupled plants, appear to be the most economical. For cargo vessels and tankers, direct-coupled Diesel plants give the greatest advantages and economies. The possibilities of higher outputs and improved economy are discussed, and the effect of the use of heavy fuel oil in Diesel engines on the relative merits of the plants is considered briefly. Some two-stroke engines of the single-acting crosshead and the double-acting types with uniflow scavenging, and examples of high-powered marine Diesel plants with these engine types for a tanker, an intermediate cargo and passenger ship, and a passenger liner are described and illustrated.&lt;br /&gt;
&lt;br /&gt;
== Volume XII, No. 5, June 1949 ==&lt;br /&gt;
&#039;&#039;&#039;Crankshaft Damping&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
The author attempts to give a correct physical explanation of natural damping by torsional vibrations, and also to obtain approximate formulae for pre-calculation of the damping in any given case. The paper describes experimental work with a single-cylinder engine driven by external power, and excited to torsional vibrations by a spring- loaded cam disk. In this way the damping from the moving parts could be investigated separately, and it was found that the damping was almost entirely due to hysteresis in the crankshaft, and oil damp­ ing, due to lateral shaft movements in the main and crankpin bearings, which was directly proportional to the bearing clearance. The paper also gives a simple and practical method for the calculation of damped vibrations in arbitrary elastic systems, and the calculation of hysteresis and bearing damping in a single-cylinder engine. Formulas are given for the total damping in multi-cylinder engines, with or without heavy flywheels, and the results are compared with the measured damping in a number of oil engines in service. &lt;br /&gt;
&lt;br /&gt;
—Paper P. Draminsky, read &lt;br /&gt;
&lt;br /&gt;
== The Modag Two-Cycle Diesel Engine ==&lt;br /&gt;
(German). &#039;&#039;Harzsa,&#039;&#039; &#039;&#039;&#039;86&#039;&#039;&#039; (1949), p. 1011 (15 Oct.).&lt;br /&gt;
&lt;br /&gt;
Small craft used to be propelled by two-stroke hot-bulb engines, which were gradually superseded by the crankcase two-cycle Diesel. In recent years a new type has been developed in Germany, the &#039;&#039;&#039;Modag-Krupp&#039;&#039;&#039; Diesel, which is at least as simple to handle and as robust as the former two types. It is an improvement on the crankcase two-cycle Diesel, its main new feature beingthe scavenging of the cylinders by means of a rotary blower. Moreover, the engine has solid fuel injection, so that the fuel consumption is low ; it is half that of the hot-bulb engines, and considerably less than that of normal engines&lt;br /&gt;
&lt;br /&gt;
with crankcase and pre-combustion chamber. The &#039;&#039;&#039;Modag&#039;&#039;&#039; Diesel is at present built with one to five cylinders, and its main structural parts are the cast-iron bed plate, the cylinder block, and the cylinder heads. Cylinder liners and pistons are made of special cast iron. The use of pressure lubrication prevents overheating of the bearings even under occasional overload. Because of its simple, robust design, this engine rapidly became popular for small German craft like coasters and trawlers. The article tabulates the main dimensions of the five engine sizes now on the market, and a diagram shows fuel consumption, engine speed, and exhaust temperature as functions of the power.&lt;br /&gt;
&lt;br /&gt;
== Comprehensive Oil Engine Research. ==&lt;br /&gt;
&#039;&#039;&#039;&#039;&#039;Gas and Oil Power, 44&#039;&#039;&#039;&#039;&#039; (1949), p. 339 (Nov.).&lt;br /&gt;
&lt;br /&gt;
The work of the British Internal Combustion Engine Research Association is described, and details are given of research work in progress and test rigs which have been developed at their laboratories. Combustion-engine roughness and knock are being studied on a &#039;&#039;&#039;Crossley&#039;&#039;&#039; BWI-17 engine, which is also used to determine the effect of different types of fuel, especially those of lower ignition quality. Investigations of torsional-vibration damping are carried out on a six-cylinder four-stroke &#039;&#039;&#039;Klockner-Humboldt-Deutz&#039;&#039;&#039; engine developing 105 b.h.p. at 1,300 r.p.m., a seismic-type of torsional vibration pick-up being attached to the front end of the crankshaft. A &#039;&#039;&#039;Petter&#039;&#039;&#039; self-induction single-cylinder two-stroke engine is used to investigate stresses in a crankweb under conditions of deliberate vertical mis-alignment of an outer bearing, and a specially designed single-cylinder engine is used for determining the cetane rating  of Diesel fuels. Investigations into the cause of crankcase explosions will be carried out on a &#039;&#039;&#039;General Motors&#039;&#039;&#039; 12-cylinder two-stroke engine, in which the original crankcase door will be replaced by a special type of safety door. A prototype bearing-testing machine has been developed for investigating the performance of bearings under the type of loading experienced in a Diesel engine big-end.&lt;br /&gt;
&lt;br /&gt;
An important part of the work is the study of crankshaft stresses, and two resonant bending-fatigue machines have been developed for this purpose. A number of foreign engines have recently been examined. A &#039;&#039;&#039;Paxman&#039;&#039;&#039; three-cylinder RPH engine is used for general study of pressure-charging effects, and the performance of highly rated engines on low-grade fuels is tested on two engines representative of latest practice.&lt;br /&gt;
&lt;br /&gt;
== New Welded Frame Engine ==&lt;br /&gt;
[[File:New_welded_fame_engine_Burmeister_Wain.png|alt=Cross section og a 1949 Burmeister &amp;amp; Wain two-stroke engine|left|thumb|428x428px|Cross section og a 1949 Burmeister &amp;amp; Wain two-stroke engine]]&lt;br /&gt;
The accompanying cross-section shows the principal details of construction of the latest type of two-stroke welded frame engine built at Copenhagen by Messrs. Burmeister and Wain. The engine in the m.s. Topeka has seven cylinders with the standard measurement of 740 mm. bore and 1,400 mm. stroke, corresponding to approximately 29 inch and 55 inch respectively. The output is 6,400 i.h.p. at 105 r.p.m., and the mechanical efficiency is in the neighbourhood of 81 per cent, giving the engine a rating of 5,200 b.h.p. which corresponds to nearly 743 b.h.p. per cylinder. The mean indicated pressure at this rating is 92Ib. per sq. in. or 6°5 kg. per sq. cm. In the case of the welded design illustrated, the bedplate, frames and scavenging air receiver are fabricated. The weight of the engine is reduced by at least 15 per cent, although the reduction may reach 25 per cent compared with cast-iron construction, depending on the type. This engine has two camshafts and there are four guides for each crosshead, and in the case of the original four-stroke B. and W. double-acting design, By using fabricated steel plates in the construction, it becomes unnecessary to carry the through-bolts which take the combustion loads down to the bottom of the bedplate. In this instance the bolts are carried from the jackets to the top of the A-frames. The exhaust takes place through a spring-loaded poppet valve centrally arranged in the cylinder cover, and scavenging air is admitted through ports uncovered by the piston at the bottom of the stroke. The air is supplied by rotary blowers, and these are driven from the crankshaft by chains and resilient couplings. It may be noted that the cylinder covers and the piston crowns are of heatresisting steel, Fresh water is used for cooling the cylinder covers and liners, the pistons being cooled by means of lubricating oil. &lt;br /&gt;
&lt;br /&gt;
There is a stuffing box with tightening rings for the air and scraper rings for the crank-chamber oil. This box is located between the scavenging-air reservoir and the crank chamber. The design allows complete separation of the lower part of the engine from the scavenging-air system, while a short piston can be utilized, with a corresponding reduction in the engine height. The length of the unit is limited by placing the scavenging-air blowers at the back and a change valve is employed for the air delivery when the direction of rotation of the crankshaft is reversed. The shop trial results showed a specific fuel consumption of 0:28lb. per ih.p. hour. Reference was made to this engine on p. 78 of Engineering Abstracts, but the design shown here represents the correct representation of the engine.&lt;br /&gt;
&lt;br /&gt;
—The Motor Ship, Vol. 30, August 1949, p. 193.&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Werkspoor Single-acting Two-stroke Engine ==&lt;br /&gt;
[[File:1949 Stork-Werkspoor.png|alt=(1949) Werkspoor|left|thumb|250x250px|(1949) Werkspoor]]&lt;br /&gt;
In Fig. 2 is illustrated a single-acting crosshead engine with multiple exhaust valves (7) in the cylinder head. The valves are Investigation of Cavitation Phenomena by Tunnel Tests moved together by a lever (8) driven from a camshaft (9). The scavengine air chamber (3) is separated from the crank chamber by a partition (20), and the lover end (25) of the liner (5) is removable, so that the piston rings may be inspected and removed without dismantling the piston, Large removable doors (27, 28) enclose the scavenging air chamber, and the bottom part (25) of the liner is lowered until it rests on the partition (20), The engine has a short piston uncovering the scavenging air ports (12). The scavenging air pump (30) is driven by levers (31) from the crosshead and is located below the level of the partition, which has an outlet (32) for the discharge of air from the pump&lt;br /&gt;
&lt;br /&gt;
—Brit, Pat, No. 616,893, issued to N.V. Werkspoor, Amsterdam. The Motor Ship, Vol. 30, September 1949, p. 244,&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Controlled Injection in High Speed Diesels ==&lt;br /&gt;
[[File:1949 CAV and Ricardo.png|alt=(1949) Nozzle|thumb|(1949) Nozzle]]&lt;br /&gt;
In a paper read by Mr. Garton of the Shell Petroleum Co,, Ltd., in Stockholm some time ago, reference is made to the knock in high speed Diesel engines with fuels of low ignition quality.  This is due to the fact that these fuels give rise to a relatively long ignition lag; hence a considerable amount of fuel has been injected into the cylinder by the time ignition starts, and it is the rapid, uncontrolled inflammation of this fuel which causes knock, One method of overcoming this difficulty, and permitting smooth operation with low cetane number fuels, is by arranging to inject only a small quantity of fuel during the earlier part of the injection period, and to increase the rate after ignition has occurred. In the Atlas system this is accomplished by the use of a two-stage cam in the fuel pump, and_a specially designed injection valve. A particular case of controlled injection is pilot injection, in which a small amount of fuel is injected before the main charge. It has already been mentioned that separate chamber engines are less sensitive to fuel ignition quality than open chamber types. The former are, however, somewhat more difficult to start at low temperatures. One method of overcoming this difficulty, without the use of heater plugs, is the Pintaux nozzle patented jointly by Messrs, C.A.V. and Messrs. Ricardo (Fig. 1) Recent experimental work has shown that the hottest zone of the separate chamber on starting is outside the normal spray path. The Pintaux nozzle is so designed that on starting (ie, at slow speeds) partial lifting of the needle valve permits a side spray of fuel into the hottest zone of the chamber (Fig. 2), thus facilitating starting. As the speed increases, the full lift of the needle valve results in most of the fuel spraying through the normal nozzle, though some delivery through the auxiliary nozzle acts as ilot charge, thus reducing combustion noise to some extent,&lt;br /&gt;
&lt;br /&gt;
—The Motor Ship, Vol. 30, August 1949, p. 201.&lt;br /&gt;
&lt;br /&gt;
== A New 4,500 B.H.P. Engine ==&lt;br /&gt;
Successful tests have been carried out by Messrs. John G. Kincaid of the first two-stroke, single-acting, crosshead design of the eccentric-type, opposed-piston, propelling engine which is being installed in the motor vessel &#039;&#039;Braeside.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
An illustrated description is given of the engine which has six cylinders 24.4 in. in diameter, the main piston stroke being 55.1 in and that of the exhaust pistons 18.5 in. Maximum continuous rating is 4,500 b.h.p. at 115 r.p.m., the mean indicated pressure being 92.4 lb/sq. in. The engine has ample width of bedplate when compared with the overall height. On account of the head-room available, the pistons and rods can be completely withdrawn vertically. The crankshaft is of the fully-built type, the webs being of cast steel.&lt;br /&gt;
&lt;br /&gt;
Integrally cast with each crankweb is an eccentric for operating the exhaust-piston gear. Each pair of eccentrics is coupled by eccentric straps and rods and four steel side rods to the cast-steel yoke of the exhaust piston. The exhaust pistons are therefore driven by, and, in turn, transmit power through the eccentrics on the crankshaft.&lt;br /&gt;
&lt;br /&gt;
The cylinders are of vanadium cast iron, cast in one piece, and are water-jacketed above the flanges by which they are bolted to the scavenge belt. The scavenge air has a clear blow-through, ensuring a fresh charge of air for each compression stroke. The scavenge air is supplied by two positive rotary blowers each driven by Renold triplex chains from the crankshaft. The fuel pumps are independent units operated by a camshaft driven by chain from the crankshaft. The main and exhaust pistons are oil-cooled and the engine is force-lubricated throughout.&lt;br /&gt;
&lt;br /&gt;
The overhauling arrangements are very complete, and the gear supplied enables maintenance work in port to be cut down to a minimum. The engine runs smoothly and quietly.&lt;br /&gt;
&lt;br /&gt;
== Opposed Piston Diesel Engine ==&lt;br /&gt;
The first &#039;&#039;&#039;Fairbanks Morse&#039;&#039;&#039; opposed piston Diesel engines were built in 1934. The first engines built attracted the attention of the U.S. Navy, and approximately three million horsepower was installed in various types of Naval vessels. As currently constructed, the engine is built in 8£ inch bore and 10 inch stroke on each piston. The engine has been built in 5, 6, 7, 8, 9 and 10 cylinder assemblies, and the makers are now beginning on a 12 cylinder engine. The most common engine is the ten cylinder size, which the U.S. Navy rated up to 2,000 h.p. at 850 r.p.m. In commercial service engines of six cylinders are rated 960 h.p., eight cylinders 1,250 h.p., ten cylinders 1,600 h.p.&lt;br /&gt;
&lt;br /&gt;
--&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1949&amp;diff=892</id>
		<title>Engineering Abstracts 1949</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1949&amp;diff=892"/>
		<updated>2026-03-28T20:30:51Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1949 =&lt;br /&gt;
&lt;br /&gt;
== Modern Trends in the Development of High-Powered Diesel Machinery ==&lt;br /&gt;
CARSTENSEN, H. &#039;&#039;Trans. Institute of Naval Architects, paper read&#039;&#039; 2 Sept. 1949.&lt;br /&gt;
&lt;br /&gt;
Typical examples are given of high-powered marine Diesel plants of more than 16,000 b.h.p. built between 1926 and 1939. Of these, the double-acting four-stroke engine has been abandoned, and the single-acting four-stroke engine is now used very little for larger ships, though it may be preferred under particularly difficult service conditions because of its simple and robust design, moreover, tests with high-pressure supercharge have shown that its output can be increased considerably. The remaining engine types mentioned are two-stroke engines, single-acting or double-acting, having either loop scavenging or uniflow scavenging. These two-stroke engine types and the four-stroke single-acting engine have been developed into fast-running units whereby any output desired can be furnished by geared or Diesel-electric plants.&lt;br /&gt;
&lt;br /&gt;
In passenger ships the arrangement of the accommodation will determine whether steam-turbine plants, fast-running Diesel engines with geared or electric transmission, or slow-running Diesel engines coupled directly to the propeller shafts will be most advantageous. The Diesel plants, particularly the direct-coupled plants, appear to be the most economical. For cargo vessels and tankers, direct-coupled Diesel plants give the greatest advantages and economies. The possibilities of higher outputs and improved economy are discussed, and the effect of the use of heavy fuel oil in Diesel engines on the relative merits of the plants is considered briefly. Some two-stroke engines of the single-acting crosshead and the double-acting types with uniflow scavenging, and examples of high-powered marine Diesel plants with these engine types for a tanker, an intermediate cargo and passenger ship, and a passenger liner are described and illustrated.&lt;br /&gt;
&lt;br /&gt;
== Volume XII, No. 5, June 1949 ==&lt;br /&gt;
&#039;&#039;&#039;Crankshaft Damping&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
The author attempts to give a correct physical explanation of natural damping by torsional vibrations, and also to obtain approximate formulae for pre-calculation of the damping in any given case. The paper describes experimental work with a single-cylinder engine driven by external power, and excited to torsional vibrations by a spring- loaded cam disk. In this way the damping from the moving parts could be investigated separately, and it was found that the damping was almost entirely due to hysteresis in the crankshaft, and oil damp­ ing, due to lateral shaft movements in the main and crankpin bearings, which was directly proportional to the bearing clearance. The paper also gives a simple and practical method for the calculation of damped vibrations in arbitrary elastic systems, and the calculation of hysteresis and bearing damping in a single-cylinder engine. Formulas are given for the total damping in multi-cylinder engines, with or without heavy flywheels, and the results are compared with the measured damping in a number of oil engines in service. &lt;br /&gt;
&lt;br /&gt;
—Paper P. Draminsky, read &lt;br /&gt;
&lt;br /&gt;
== The Modag Two-Cycle Diesel Engine ==&lt;br /&gt;
(German). &#039;&#039;Harzsa,&#039;&#039; &#039;&#039;&#039;86&#039;&#039;&#039; (1949), p. 1011 (15 Oct.).&lt;br /&gt;
&lt;br /&gt;
Small craft used to be propelled by two-stroke hot-bulb engines, which were gradually superseded by the crankcase two-cycle Diesel. In recent years a new type has been developed in Germany, the &#039;&#039;&#039;Modag-Krupp&#039;&#039;&#039; Diesel, which is at least as simple to handle and as robust as the former two types. It is an improvement on the crankcase two-cycle Diesel, its main new feature beingthe scavenging of the cylinders by means of a rotary blower. Moreover, the engine has solid fuel injection, so that the fuel consumption is low ; it is half that of the hot-bulb engines, and considerably less than that of normal engines&lt;br /&gt;
&lt;br /&gt;
with crankcase and pre-combustion chamber. The &#039;&#039;&#039;Modag&#039;&#039;&#039; Diesel is at present built with one to five cylinders, and its main structural parts are the cast-iron bed plate, the cylinder block, and the cylinder heads. Cylinder liners and pistons are made of special cast iron. The use of pressure lubrication prevents overheating of the bearings even under occasional overload. Because of its simple, robust design, this engine rapidly became popular for small German craft like coasters and trawlers. The article tabulates the main dimensions of the five engine sizes now on the market, and a diagram shows fuel consumption, engine speed, and exhaust temperature as functions of the power.&lt;br /&gt;
&lt;br /&gt;
== Comprehensive Oil Engine Research. ==&lt;br /&gt;
&#039;&#039;&#039;&#039;&#039;Gas and Oil Power, 44&#039;&#039;&#039;&#039;&#039; (1949), p. 339 (Nov.).&lt;br /&gt;
&lt;br /&gt;
The work of the British Internal Combustion Engine Research Association is described, and details are given of research work in progress and test rigs which have been developed at their laboratories. Combustion-engine roughness and knock are being studied on a &#039;&#039;&#039;Crossley&#039;&#039;&#039; BWI-17 engine, which is also used to determine the effect of different types of fuel, especially those of lower ignition quality. Investigations of torsional-vibration damping are carried out on a six-cylinder four-stroke &#039;&#039;&#039;Klockner-Humboldt-Deutz&#039;&#039;&#039; engine developing 105 b.h.p. at 1,300 r.p.m., a seismic-type of torsional vibration pick-up being attached to the front end of the crankshaft. A &#039;&#039;&#039;Petter&#039;&#039;&#039; self-induction single-cylinder two-stroke engine is used to investigate stresses in a crankweb under conditions of deliberate vertical mis-alignment of an outer bearing, and a specially designed single-cylinder engine is used for determining the cetane rating  of Diesel fuels. Investigations into the cause of crankcase explosions will be carried out on a &#039;&#039;&#039;General Motors&#039;&#039;&#039; 12-cylinder two-stroke engine, in which the original crankcase door will be replaced by a special type of safety door. A prototype bearing-testing machine has been developed for investigating the performance of bearings under the type of loading experienced in a Diesel engine big-end.&lt;br /&gt;
&lt;br /&gt;
An important part of the work is the study of crankshaft stresses, and two resonant bending-fatigue machines have been developed for this purpose. A number of foreign engines have recently been examined. A &#039;&#039;&#039;Paxman&#039;&#039;&#039; three-cylinder RPH engine is used for general study of pressure-charging effects, and the performance of highly rated engines on low-grade fuels is tested on two engines representative of latest practice.&lt;br /&gt;
&lt;br /&gt;
== New Welded Frame Engine ==&lt;br /&gt;
[[File:New_welded_fame_engine_Burmeister_Wain.png|alt=Cross section og a 1949 Burmeister &amp;amp; Wain two-stroke engine|left|thumb|428x428px|Cross section og a 1949 Burmeister &amp;amp; Wain two-stroke engine]]&lt;br /&gt;
The accompanying cross-section shows the principal details of construction of the latest type of two-stroke welded frame engine built at Copenhagen by Messrs. Burmeister and Wain. The engine in the m.s. Topeka has seven cylinders with the standard measurement of 740 mm. bore and 1,400 mm. stroke, corresponding to approximately 29 inch and 55 inch respectively. The output is 6,400 i.h.p. at 105 r.p.m., and the mechanical efficiency is in the neighbourhood of 81 per cent, giving the engine a rating of 5,200 b.h.p. which corresponds to nearly 743 b.h.p. per cylinder. The mean indicated pressure at this rating is 92Ib. per sq. in. or 6°5 kg. per sq. cm. In the case of the welded design illustrated, the bedplate, frames and scavenging air receiver are fabricated. The weight of the engine is reduced by at least 15 per cent, although the reduction may reach 25 per cent compared with cast-iron construction, depending on the type. This engine has two camshafts and there are four guides for each crosshead, and in the case of the original four-stroke B. and W. double-acting design, By using fabricated steel plates in the construction, it becomes unnecessary to carry the through-bolts which take the combustion loads down to the bottom of the bedplate. In this instance the bolts are carried from the jackets to the top of the A-frames. The exhaust takes place through a spring-loaded poppet valve centrally arranged in the cylinder cover, and scavenging air is admitted through ports uncovered by the piston at the bottom of the stroke. The air is supplied by rotary blowers, and these are driven from the crankshaft by chains and resilient couplings. It may be noted that the cylinder covers and the piston crowns are of heatresisting steel, Fresh water is used for cooling the cylinder covers and liners, the pistons being cooled by means of lubricating oil. &lt;br /&gt;
&lt;br /&gt;
There is a stuffing box with tightening rings for the air and scraper rings for the crank-chamber oil. This box is located between the scavenging-air reservoir and the crank chamber. The design allows complete separation of the lower part of the engine from the scavenging-air system, while a short piston can be utilized, with a corresponding reduction in the engine height. The length of the unit is limited by placing the scavenging-air blowers at the back and a change valve is employed for the air delivery when the direction of rotation of the crankshaft is reversed. The shop trial results showed a specific fuel consumption of 0:28lb. per ih.p. hour. Reference was made to this engine on p. 78 of Engineering Abstracts, but the design shown here represents the correct representation of the engine.&lt;br /&gt;
&lt;br /&gt;
—The Motor Ship, Vol. 30, August 1949, p. 193.&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Werkspoor Single-acting Two-stroke Engine ==&lt;br /&gt;
[[File:1949 Stork-Werkspoor.png|alt=(1949) Werkspoor|left|thumb|250x250px|(1949) Werkspoor]]&lt;br /&gt;
In Fig. 2 is illustrated a single-acting crosshead engine with multiple exhaust valves (7) in the cylinder head. The valves are Investigation of Cavitation Phenomena by Tunnel Tests moved together by a lever (8) driven from a camshaft (9). The scavengine air chamber (3) is separated from the crank chamber by a partition (20), and the lover end (25) of the liner (5) is removable, so that the piston rings may be inspected and removed without dismantling the piston, Large removable doors (27, 28) enclose the scavenging air chamber, and the bottom part (25) of the liner is lowered until it rests on the partition (20), The engine has a short piston uncovering the scavenging air ports (12). The scavenging air pump (30) is driven by levers (31) from the crosshead and is located below the level of the partition, which has an outlet (32) for the discharge of air from the pump&lt;br /&gt;
&lt;br /&gt;
—Brit, Pat, No. 616,893, issued to N.V. Werkspoor, Amsterdam. The Motor Ship, Vol. 30, September 1949, p. 244,&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Controlled Injection in High Speed Diesels ==&lt;br /&gt;
[[File:1949 CAV and Ricardo.png|alt=(1949) Nozzle|thumb|(1949) Nozzle]]&lt;br /&gt;
In a paper read by Mr. Garton of the Shell Petroleum Co,, Ltd., in Stockholm some time ago, reference is made to the knock in high speed Diesel engines with fuels of low ignition quality.  This is due to the fact that these fuels give rise to a relatively long ignition lag; hence a considerable amount of fuel has been injected into the cylinder by the time ignition starts, and it is the rapid, uncontrolled inflammation of this fuel which causes knock, One method of overcoming this difficulty, and permitting smooth operation with low cetane number fuels, is by arranging to inject only a small quantity of fuel during the earlier part of the injection period, and to increase the rate after ignition has occurred. In the Atlas system this is accomplished by the use of a two-stage cam in the fuel pump, and_a specially designed injection valve. A particular case of controlled injection is pilot injection, in which a small amount of fuel is injected before the main charge. It has already been mentioned that separate chamber engines are less sensitive to fuel ignition quality than open chamber types. The former are, however, somewhat more difficult to start at low temperatures. One method of overcoming this difficulty, without the use of heater plugs, is the Pintaux nozzle patented jointly by Messrs, C.A.V. and Messrs. Ricardo (Fig. 1) Recent experimental work has shown that the hottest zone of the separate chamber on starting is outside the normal spray path. The Pintaux nozzle is so designed that on starting (ie, at slow speeds) partial lifting of the needle valve permits a side spray of fuel into the hottest zone of the chamber (Fig. 2), thus facilitating starting. As the speed increases, the full lift of the needle valve results in most of the fuel spraying through the normal nozzle, though some delivery through the auxiliary nozzle acts as ilot charge, thus reducing combustion noise to some extent,&lt;br /&gt;
&lt;br /&gt;
—The Motor Ship, Vol. 30, August 1949, p. 201.&lt;br /&gt;
&lt;br /&gt;
== A New 4,500 B.H.P. Engine ==&lt;br /&gt;
Successful tests have been carried out by Messrs. John G. Kincaid of the first two-stroke, single-acting, crosshead design of the eccentric-type, opposed-piston, propelling engine which is being installed in the motor vessel &#039;&#039;Braeside.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
An illustrated description is given of the engine which has six cylinders 24.4 in. in diameter, the main piston stroke being 55.1 in and that of the exhaust pistons 18.5 in. Maximum continuous rating is 4,500 b.h.p. at 115 r.p.m., the mean indicated pressure being 92.4 lb/sq. in. The engine has ample width of bedplate when compared with the overall height. On account of the head-room available, the pistons and rods can be completely withdrawn vertically. The crankshaft is of the fully-built type, the webs being of cast steel.&lt;br /&gt;
&lt;br /&gt;
Integrally cast with each crankweb is an eccentric for operating the exhaust-piston gear. Each pair of eccentrics is coupled by eccentric straps and rods and four steel side rods to the cast-steel yoke of the exhaust piston. The exhaust pistons are therefore driven by, and, in turn, transmit power through the eccentrics on the crankshaft.&lt;br /&gt;
&lt;br /&gt;
The cylinders are of vanadium cast iron, cast in one piece, and are water-jacketed above the flanges by which they are bolted to the scavenge belt. The scavenge air has a clear blow-through, ensuring a fresh charge of air for each compression stroke. The scavenge air is supplied by two positive rotary blowers each driven by Renold triplex chains from the crankshaft. The fuel pumps are independent units operated by a camshaft driven by chain from the crankshaft. The main and exhaust pistons are oil-cooled and the engine is force-lubricated throughout.&lt;br /&gt;
&lt;br /&gt;
The overhauling arrangements are very complete, and the gear supplied enables maintenance work in port to be cut down to a minimum. The engine runs smoothly and quietly.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1946</title>
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&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
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= Engineering Abstracts from 1946 =&lt;br /&gt;
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== German Wartime Technical Developments. ==&lt;br /&gt;
SCHADE, H. A., Commodore, U.S.N. Society of Naval Architects and Marine Engineers (New York), paper read at Annual Meeting, 14th November, 1946.&lt;br /&gt;
&lt;br /&gt;
A general description is given of certain selected items in Germany which have been reported by the U.S. Naval Technical Mission in Europe. The author&#039;s remarks fall under the following headings :-&lt;br /&gt;
&lt;br /&gt;
Submarines. The Type VllC submarine, of conventional design, was built in large numbers during the war. Of the revolutionary Type XXI, 119 were completed, but none went out on war service. This type was designed as a highly-manoeuvrable high-speed vessel, which could remain submerged for long periods and operate at greater depths than most submarines. The sukmerged speed was 18 knots, and the surface speed 16 knots with super-chargers and somewhat less without them ; back pressure in the Schnorchel (breathing-tube) prevented the engines from attaining their rated capacity, so the superchargers were removed as the Schnorchel was indispensable. Trouble with the hydraulic system, which was far more extensive than is usual in submarines, was a major defect of Type XXI. These vessels, about 250 ft. long and with all-welded hulls, were prefabricated in nine sections which were welded together.&lt;br /&gt;
&lt;br /&gt;
Surface Vessels. The all-welded triple-screw battleships Bismarck and Tirpitz were 821 ft. long, had load displacements of 52,700 tons, and were propelled at 30 knots by three sets of geared-turbine machinery totalling 150,000 s.h.p. A design known as battleship &amp;quot;H&amp;quot; was developed, and construction was started, but plans were changed frequently. Originally 910 ft. long, 56,400 tons displacement, and 30 knots on three shafts, each having four Diesels of 12,500 s.h.p. per engine, the ultimate design was 1,132 ft. long, 141,500 tons displacement, and 30 knots on four shafts, two with four Diesels each totalling 60,000 s.h.p. per shaft, and two shafts each with geared turbines of 80,000 s.h.p. per shaft. The Prinz Eugen, 692 ft. long with a load displacement of 19,500 tons and a speed of 32.5 knots, was fitted with anti-rolling tanks, and was propelled by three geared-turbine sets. The S-38, a Diesel-propelled wooden-hulled 45-knot torpedo boat, had special side rudders for decreasing the required power at high speeds.&lt;br /&gt;
&lt;br /&gt;
Turbines and Gears. In general, the German turbine propulsion equipment was inferior to similar American machinery. The policy of using single reduction gearing with three or four pinions meshing with the main gear resulted in low turbine speeds and high specific weights. Turbine design and manufacture were mediocre, and there was poor utilisation of energy in the heat cycle ; the steam conditions should have produced high propulsion efficiencies. Some specific plants are discussed.&lt;br /&gt;
&lt;br /&gt;
Diesel Engines. The six-cylinder and twenty-four cylinder M.A.N. were well-developed and reliable. The Daimler-Benz Model MB 511 is an outstanding four-cycle supercharged lightweight Diesel for naval craft ; on a continuous rating of 1,980 b.h.p. at 1,480 r.p.m., the bare engine weight is 4.4 lb/lb.h.p.&lt;br /&gt;
&lt;br /&gt;
The Hamburg Model Basin. A large variable-pressure cavitation water tunnel and a smaller tunnel were constructed, but were completed too late to be used. A new towing carriage, an extended towing basin, and a new manoeuvring basin were under construction. &lt;br /&gt;
&lt;br /&gt;
An appendix lists the relevant Naval Technical Mission Reports.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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[[Engineering Abstracts 1970]]&lt;/div&gt;</summary>
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== Large Nine-cylinder Diesel Engine ==&lt;br /&gt;
A nine-cylinder engine designed to develop 11,200 b.h.p. at 115 r.p.m. under normal conditions at sea has recendy been completed by Burmeister and Wain. It has cylinders 740 mm. in diameter with a piston stroke of 1,600 mm., and is to be installed in a tanker under construction at the Nakskov Skibsvaerft for A.P. Moller, Copenhagen. It is the highest-powered marine engine constructed by Burmeister and Wain.&lt;br /&gt;
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The new engine is equipped with three turbochargers of the Brown-Boveri VTR-630 type, these blowers being similar to those employed in the main engines of A. P. Moller’s M.S. &#039;&#039;Dorthe Maersk&#039;&#039; and the &#039;&#039;Songkhla, Samoa&#039;&#039; and &#039;&#039;Sibonga&#039;&#039; of the East Asiatic Co. The output of the 11,200 b.h.p. engine is slightly higher than that of a corresponding 12-cylinder non-turbo-charged unit, which is about 10 feet 10 inches longer and 35 per cent heavier than the nine-cylinder turbo-charged engine. Ten nine-cylinder engines of this type are being built by Burmeister and Wain and one with 10 cylinders, for a cargo ship, at Eriksbergs Mek. Verk. developing 12,500 b.h.p. In Japan an engine has been installed in the recently completed &#039;&#039;Hanmasan Maru,&#039;&#039; a cargo ship of 10,200 tons with a service speed of 17} knots. The fuel consumption of these engines, based upon the results of similar but smaller units installed in ships now in service is expected to be 0 3341b. per b.h.p. hr., the mechanical efficiency being about 88 per cent. In normal service the mean indicated pressure is approximately 1021b. per sq. in.&lt;br /&gt;
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—&#039;&#039;The Motor Ship, March 1954; Vol. 34, p. 518.&#039;&#039;&lt;br /&gt;
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== Cas Turbine Progress ==&lt;br /&gt;
Marine auxiliary and industrial gas turbines ranging in power from 140 to 900 kW are being developed at Bedford by W. H. Allen, Sons and Co., Ltd. Of the four basic designs involved, the smallest is an all-radial-flow single-shaft unit with a rating of 200 b.h.p. (140 kW) at an air inlet temperature of 60 deg. F. (15 deg. C .); the prototype is now undergoing extensive testing and development. Designed originally at the request of the Admiralty, this small engine is intended for any duty where low fuel consumption is of less importance than such advantages as light weight, compactness, quick starting, rapid acceptance of load, and absence of cooling water. An ingenious feature is the use of a one-piece turbo-compressor rotor, with the centrifugal impeller vanes machined from one face of a forged steel disc and the centripetal turbine vanes from the other. By thus taking the familiar back-to-back arrangement of radial-flow components to its logical conclusion, the opportunity is presented of cooling the turbine by direct heat transfer across the rotor disc. The Allen designers have applied this principle so successfully that the ferritic steel disc of the prototype engine shows every sign of lasting for many thousands of running hours despite the use of inlet gas temperatures up to 800 deg. C. (1,470 deg. F.). A larger gas turbine of familiar type to the 200-b.h.p. unit has been designed, and manufacture will commence shortly. Six d.c. generator-driving versions of it have been ordered by the Alfred H olt shipping concern for auxiliary use aboard Blue Funnel liners, the rating being 350 kW at an air inlet temperature of 85 deg. F. (30 deg. C.). These sets are too large to make efficient use of a radial-flow turbine, so the single-stage centrifugal impeller is driven in each case by a two-stage axial turbine. On behalf of the Admiralty, the company is designing and constructing two interesting gas-turbo-alternators rated at 500 kW in tropical conditions. No details have yet been released for publication.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Oil Engine and Gas Turbine, March 1954; Vol. 21, p. 436.&#039;&#039;&lt;br /&gt;
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== Centripetal Turbine tor High Specific Outputs ==&lt;br /&gt;
In 1939 the U.S. Navy Department requested bids on two 2,500-h.p. propulsion turbines for the Navy submarine chaser PC-452. The author’s Company was awarded the contract on the basis of the evaluation made by the U.S. Navy Department, which took into consideration the weight of the turbines, their overall dimensions, and their efficiency. The Company’s design study resulted in the choice of a compound turbine arrangement—this is, a high-pressure and a separate low-pressure turbine for each of the two propelling units. It also indicated that it was necessary to operate these turbines at no less than 15,000 r.p.m. if the design target (with regard to bulk, weight, and efficiency) was to be met. This high speed ruled out the axial-flow wheel for the last stage of the low-pressure turbine, because this type is incapable of passing the large volume flows at such high r.p.m., without prohibitively low efficiency. The high-specific-speed centripetal turbine came to the rescue, and was used not only in the last stage but also in the next-to-last stage of the low-pressure turbine,&lt;br /&gt;
&lt;br /&gt;
a sectional view of which is shown in Fig. 10. This particular application of the high-specific-speed centripetal turbine made possible the attainment of a specific weight, for the complete unit, of only slightly over 31b.-per-shaft horsepower, including the double reduction gear, turning gear, and other accessories. This specific weight is by far the lowest that has ever been achieved for a marine propelling steam turbine. The units fully met the efficiency guarantees, and their small dimensions made it possible to accommodate them easily in the confined space of the slender hull. Several different sizes of turbosuperchargers for Diesel engines have been constructed in the past four years by the author’s Company. In the course of the development of these units it has been clearly demonstrated that the high-specific-speed centripetal turbine wheel is the ideal answer for this application for the following reasons: 1. This turbine is capable of an r.p.m. sufficiently high to bring the compressor driven by it into a specific speed range where maximum compressor efficiency can be obtained. An axial-flow turbine designed for the same flow and stress conditions would have to operate at lower r.p.m., which would result in a correspondingly lower specific speed of the compressor, thus preventing the attainment of maximum possible compressor efficiency. 2. Under the particular flow and operating conditions encountered in the service of exhaust turbines for Diesel engines, distinctly higher turbine efficiency can be obtained with the centripetal turbine than is possible with the axial-flow type. 3. The efficiency of the centripetal turbine, which in itself is high, can be further increased by the recovery of kinetic energy in the turbine exhaust through the use of an exhaust diffuser in the form of a simple conical duct. 4. The centripetal turbine, owing to its low number of husky blades, is far less delicate than the axial-flow wheel and better able to cope with the severe service of Diesel-engine exhaust gas operation. In addition thereto, it is cheaper to manufacture. 5. The turbine blades and turbine rotor hub can be cooled in a simple manner, similar to the one described for the aircraft exhaust gas turbines. This reduces the metal temperatures even under the extreme conditions of Diesel-engine preturbine temperature encountered during engine overload conditions, to values which permit designing for virtually unlimited time to rupture. 6. The inertia of the centripetal wheel is lower than that of an equivalent axial-flow wheel, which results in a more rapid change of turbo-supercharger speed with a change in engine load. 7. The stationary turbine nozzles, directing the flow into the centripetal wheel, can be arranged between parallel radial walls, which makes it practicable to provide for pivoting the guide vanes to adjust the nozzle areas and angles for matching the turbo-supercharger to the engine.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;R. Birmunn, Transactions of the A.S.M.E., February 1954; Vol. 76, pp. 173-187.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Motorships for South America ==&lt;br /&gt;
Canadian Vickers, Ltd., of Montreal is again delivering ships to The Flota Mercante Grancolombiana. First two of a series of four additional motorships, the &#039;&#039;Ciudad de Valencia&#039;&#039; and &#039;&#039;Ciudad de Cali,&#039;&#039; have been in service several months. The other two vessels, the &#039;&#039;Ciudad de Ibague&#039;&#039; and &#039;&#039;Ciudad de Cumana&#039;&#039; will be delivered in the forthcoming months. In accord with their building programme, Flota Mercante Grancolombiana, S.A., placed orders with Canadian Vickers, Ltd. for the construction of these four new vessels to augment their very fast cargo carrying service between the major ports of Venezuela, Colombia, Ecuador, New Orleans, New York and Montreal. Each ship is propelled by a single Nordberg six-cylinder Diesel engine, rated 4,275 b.h.p. at 160 r.p.m., direct connected to&lt;br /&gt;
&lt;br /&gt;
the propeller shaft. The engine has a 29in. bore by a 40in. stroke and is of the two-cycle, single-acting type with port scavenging and port exhaust. The propulsion Diesel is independently scavenged by two motor-driven blowers each of 200 h.p. rating, taking air from the engine room through a Maxim silencer and each discharging 10,000 cfm. at about 2 -41b. per sq. in. discharge pressure to a common intake manifold. This method of obtaining scavenge air results in a shorter engine, and in case of failure of one of the blowers, the engine is still capable of maintaining 70 per cent ship speed with the remaining blower. The main engine control platform is at the after end of the engine on the port side and the log desk, engine telegraph, instrument panel, alarm panel, telephone booth are all disposed conveniently around the operator and are actuated by automatic controls. They have an actual air delivery of 68 cfm. at 870 r.p.m. and are of the two-stage type, water cooled and fitted with inter and after cooler. Auxiliary power on each of the vessels is supplied by three Nordberg four-cycle, eight-cylinder inter-cooled-super-charged Diesel engines. These engines are of the single-acting, trunk piston, mechanical injection type with cylinders of 9in. bore and ll^in . stroke rated 580 h.p. at 600 r.p.m. Each drives a 400 kW. 120/240 volt, 3 phase Westinghouse generator arranged for parallel operation and capable of carrying a 25 per cent out of balance current.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;D. Shearing, Diesel Progress, December 1953; Vol. 19, pp. 42-43.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Diesel-electric Tanker ==&lt;br /&gt;
The accompanying illustration shows one of the two Diesel-electric propelling motors of 1,750 h.p. at 128 r.p.m. in the 9,300-tons Soviet tanker &#039;&#039;General Asi Aslanow.&#039;&#039; The motors are supplied with direct current at 700 volts from four 700 kW. D.C. generators, each driven by a supercharged six-cylinder four-stroke cycle Diesel engine at 900 b.h.p. at 720 r.p.m. Cylinder diameter is 308 mm. and stroke is 330 mm. The pistons are of light alloy and are not liquid cooled.&lt;br /&gt;
&lt;br /&gt;
—S. &#039;&#039;Antonow, Schiffbautechnik, December 1953; Vol. 3, pp. 359-362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cas Turbined Coaster ==&lt;br /&gt;
The first merchant vessel to be equipped with propelling machinery consisting of gas turbines fed by free-piston gas generators has recently completed her sea trials. This coaster, the &#039;&#039;Cantenac,&#039;&#039; is one of two vessels of the same type ordered by the French Ministry of Merchant Marine on behalf of Worms &amp;amp; Cie., from the Chantiers et Ateliers Augustin Norm and at Le Havre, as war loss replacement. &lt;br /&gt;
&lt;br /&gt;
The &#039;&#039;Cantenac&#039;&#039; is a vessel of 850 tons with three holds and has her propelling machinery arranged aft. She is 185 feet in length b.p., 30 feet 6 inches moulded breadth, 14 feet 5 inches moulded depth to main deck, and has a mean draught of 13 feet 6 inches. &lt;br /&gt;
&lt;br /&gt;
The propelling machinery consists of two Pescara-SIGMA type GS-34 free-piston gas generators; two gas turbines connected to a reduction gear, each fed by one gas generator; and a double reduction gear connecting the turbines to a single shaft and reducing the number of revolutions to 220 r.p.m. The complete design of this vessel, both hull and engines, has been carried out by the shipbuilders. &#039;&#039;Saving in Weight.&#039;&#039; The free-piston gas generator operates on the two-stroke cycle and consists of a horizontal cylinder with two opposed pistons, each of which is directly connected to a compressor piston. The outer part of the compressor cylinder constitutes a compensating cushion. The mixture of exhaust gas and scavenge air forms the gas which is used to drive the turbine. A comparison of the weight of a gas generator installation compared with that of a corresponding Diesel installation is in favour of the former scheme. A typical four-stroke Diesel engine, developing 1,800 h.p. at 220 r.p.m., and with 40 per cent supercharge, weighs about 1261b. per h.p., whereas a gas generator installation consisting of two GS-34 generators, one turbine and reducion gear of the same power and speed, is about 891b. per h.p. The saving in weight and bulk is only one advantage. &lt;br /&gt;
&lt;br /&gt;
There is also flexibility of operation, avoidance of vibration, ease of maintenance and low starting air consumption. It is claimed that in all probability the free-piston gas generator unit will become the engine with the highest thermal efficiency, with a specific fuel consumption referred to the turbine shaft of less than 0-331b. per s.h.p. per hr. At the moment it is in the region of 0 391b. per s.h.p. per hr., a figure not far different from the consumption of 0-331b. per b.h.p. per hr. obtained from a supercharged two-stroke Diesel engine. Trials were run on 19th January on fuel No. 1, which corresponds to a Redwood viscosity of about 950 secs, at 100 deg. F. The unit is designed to run on both distillator and light residual fuel.&lt;br /&gt;
&lt;br /&gt;
The engine was run with two gas generators developing 1,200 h.p. on one trial and with one only developing 700 h.p. on another. It is understood that the tests were highly satisfactory and it was found possible to establish, in particular, the ease and speed of manoeuvrability of the propelling machinery, as well as the ease with which one fuel was substituted for another.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 17th February 1954; Vol. 130, p. 213.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Free Piston Cas Generators ==&lt;br /&gt;
The Baldwin-Lima-Hamilton free piston generator development was conducted under a (U.S.) Navy Department contract to obtain a unit suitable for naval-combatant requirements. Consequently, it was designed with a view toward high specific output, reasonably low weight, and compactness, and to provide high thermal efficiency and reliability. In other words, to fulfil its purpose, it had to compete favourably with the thermal efficiency of modern Diesel engines and give the added advantages of simplicity, low initial cost, and smooth vibrationless operation. &#039;I&#039;he power plant constructed was a twin unit with two gas generators supplying gas to a single turbine and reduction gear. It is outward-compression with both direct-bounce and reverse-bounce cylinders for control. The two gas generators are synchronized to reduce pulsations of the gas to the turbine and they can be operated together or singly, as the load requirements necessitate. The principal specifications are given as follows: —-&lt;br /&gt;
&lt;br /&gt;
Table 2.—B-L-H Model B Gas Generator Specifications&lt;br /&gt;
&lt;br /&gt;
Power-cylinder bore, inches ... ... 8 ¼&lt;br /&gt;
&lt;br /&gt;
Compressor-cylinder bore, inches ... 23&lt;br /&gt;
&lt;br /&gt;
Direct-bounce-cylinder bore, inches ... 8 ¼&lt;br /&gt;
&lt;br /&gt;
Reverse-bounce-cylinder bore, inches... 23&lt;br /&gt;
&lt;br /&gt;
Piston stroke (full load), inches ... 11&lt;br /&gt;
&lt;br /&gt;
Cyclic frequency (maximum), cycles per min. ... ... ... ... 1,035&lt;br /&gt;
&lt;br /&gt;
Exhaust pressure to turbine, lb. per sq. in. gauge ... ... ... ... 90&lt;br /&gt;
&lt;br /&gt;
Exhaust temperature to turbine, deg. F. 1,295&lt;br /&gt;
&lt;br /&gt;
Gas horsepower (maximum) ... ... 885&lt;br /&gt;
&lt;br /&gt;
The complete power plant, after completion of its acceptance trials at the builders’ plant, was sent to the U.S. Naval Engineering&lt;br /&gt;
&lt;br /&gt;
Experiment Station at Annapolis, Md., in 1950, for further test and evaluation. The principal data obtained during 700 hours of test operation are presented. Fig. 11 shows the gas-generator output, based on adiabatic expansion of the gas. The output pressure to the turbine was carried to 901b. per sq. in. gauge as contrasted with 501b. per sq. in. gauge for the French SIGM A Model GS-34. Of course, the relation of horsepower output to exhaust pressure is mainly a function of the size and characteristics of the turbine used in these tests. The curve shows outputs up to 1,770 gas-horsepower with the 901b. per sq. in. gauge maximum pressure to the turbine. On later accelerated tests to determine piston-ring and cylinder-liner suitability, where more severe operating conditions were imposed without a turbine, the same output was reached with only 701b. per sq. in. gauge exhaust pressure and the same exhaust temperature. This was a result of increasing the effective orifice area because the turbine used has a smaller equivalent orifice. The gas-horsepower curve in Fig. 11 shows that the output is increasing without any decrease in rate up to the limiting exhaust temperature and pressure set by this particular design. The shaft-horsepower curve in Fig. 11 is based on the desired 85 per cent efficiency for turbine and reduction gear, as it was in the SIGMA data. T hat efficiency&lt;br /&gt;
&lt;br /&gt;
was not reached with the turbine used on the actual tests. However, turbines are available with peak efficiency of 85 per cent or higher. The shaft-horsepower curve is corrected for the power requirement of the auxiliary equipment which cannot be driven directly from the turbine. Thus about 1,420 s.h.p. is available from an installation with a weight and space no greater than that of current Diesel installations and less than that of other types of power plants having comparable thermal efficiency. The model now under development at B-L-H is much smaller and lighter. Fig. 12 shows the measured fuel consumption on a gas-horsepower basis and those calculated for a possible turbine efficiency of 85 per cent. The maximum thermal efficiency of 40 3 per cent at the gasifier discharge is very satisfactory and compares favourably with the SIGMA maximum of 3 8 2 per cent. This increase in thermal efficiency&lt;br /&gt;
&lt;br /&gt;
is to be expected in view of higher operating conditions. The correction to a shaft-horsepower basis shows a greater reduction than was made for the SIGM A design because exact information was available on the B-L-H power plant and deduction was made for all losses, including supply of auxiliary control air, cooling-water pumping, and similar power expenditures.&lt;br /&gt;
&lt;br /&gt;
The only deduction made for the SIGM A unit was based on turbine efficiency of 85 per cent. It is not known if the previously published data include corrections for power to auxiliary equipment. After making these corrections to a minimum shaft-horsepower basis, the thermal efficiency is still 32’3 per cent. The turbine was rated at a maximum inlet temperature of 1,350 deg. F. However, the peak pressure of 901b. per sq. in. gauge was reached with less than 1,300 deg. F. As stated before, without the turbine and with a variation in the gas pressure-to-orifice relationship, the same temperature gave as much load with only 701b. per sq. in. gauge exhaust-gas pressure.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;J. J. McMullen and W. G. Payne, Transactions of the A.S.M.E., January 1954; Vol. 76, pp. 1-14.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Medium Speed Four-stroke Engine ==&lt;br /&gt;
[[File:1954 MAN drawing.png|left|thumb|398x398px|&#039;&#039;Sectional elevation of four-stroke M.A.N. engine&#039;&#039;]]&lt;br /&gt;
A feature of German post-war shipping has been the increasing number of ships propelled by either direct-coupled or geared M.A.N. four-stroke Diesel engines. These are m anufactured with exhaust-gas pressure-charging or as normally-aspirated units, the supercharged units having the relatively conservative mean effective pressure of 9 1 kg. per sq. cm. (129 per sq. in.). It is known, of course, that the Maschinenfabrik Augsburg Nurnberg A.G. has been actively pursuing the development of the highly supercharged four-stroke engine, the results of which have been previously published. &lt;br /&gt;
&lt;br /&gt;
Such engines, designed for, and operating on, higher pressures, have not yet been put into commercial service, although some are now on order, but there is, nevertheless, much of interest in the current design. This is an engine with a cylinder diameter of 400 mm. and a piston stroke of 600 mm., which, as a six-cylinder unit without supercharging, will develop 785 b.h.p. at 275 r.p.m., the corresponding piston speed being 5 5 m. per sec. The engine, which is also designed for industrial duties, is built with from five to ten cylinders—with and without pressure charging. Normal supercharging amounts to about 60 per cent, corresponding to an m.e.p. of 91 kg. per sq. cm., so that a 10-cylinder engine supercharged to this extent develops about 2,100 h.p. This is the continuous rating and does not include a 10 per cent overload allowance. A feature of the design is that arrangements have been made whereby a drive can also be taken from the forward end, if desired; this is particularly advantageous in such vessels as ferries, or for fishing boats where a drive is generally required for the trawl winch or winch generator.&lt;br /&gt;
&lt;br /&gt;
The exhaust-gas turbo-blower is of the standard M.A.N. design with self-aligning bearings of the multi-surface type between the turbine rotor and the blower, to ensure the minimum of friction. The construction of the engine is generally simple. The welded bedplate supports the columns and the cylinder block which, for the larger engines, comprises a number of units bolted together. Cast integral with the cylinder block is the air suction manifold which supports the camshaft seating and the fuel pumps. It will be seen that the arrangement of the camshaft is such that the need for push rods is obviated.  &lt;br /&gt;
&lt;br /&gt;
The drive for the camshaft is by means of a 2J-in. simplex chain. W ith four-stroke engines of similar size, reversing is generally effected in three stages, the push rods being lifted from and replaced on the cams in the first and third stages; the camshaft is moved to its requisite position during the second phase. W ith this engine, however, all cams have oblique surfaces, so that it is not necessary to lift the rollers from the cams, an arrangement which enables a simplification of the reversing gear and ensures a quicker response. Owing to the excellent heat transmission properties of the aluminium alloy of which the pistons are composed, the pistons are uncooled.&lt;br /&gt;
&lt;br /&gt;
With 60 per cent supercharging, the temperature at the centre of the piston crown, measured by thermo-elements 6 mm. below its surface, remains below 210 deg. C. The temperature within the vicinity of the topmost piston ring is about 20 deg. lower—about 190 deg. C. at the same load—at which temperature sticking of piston rings should not be encountered. An interesting point about the pistons is that they are ground spherically from the bottom to the top, i.e. with a smaller diameter at the bottom and top than in the middle. Furthermore, the pistons are ground slightly oval in their cross-section, the degree of ovalness increasing from the bottom upwards to about the top piston ring, where the cross section gradually reverts to round form.&lt;br /&gt;
&lt;br /&gt;
— &#039;&#039;The Motor Ship, February 1954; Vol. 34, pp. 486-487&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Diesel Engine Synchronization ==&lt;br /&gt;
[[File:1954 Diesel engine syncro fig 1.png|alt=FIG. 1-Applications of the synchronizer. 1. Main engine; 2. electro-magnetic coupling; 3. gearing; 4. synchronizer|left|thumb|250x250px|FIG. 1-Applications of the synchronizer. 1. Main engine; 2. electro-magnetic coupling; 3. gearing; 4. synchronizer]]&lt;br /&gt;
The purpose of synchronizing is to obtain a fixed relative position of two rotating shafts. In a marine Diesel propelled installation this can be of value by removing, or at least reducing, disturbing vibrations which may occur in consequence of unbalanced inertia moments of the crankshafts, or resulting from a disadvantageous relative position of the rotating propeller blades. The &#039;&#039;&#039;De Schelde&#039;&#039;&#039; synchronizer, which has been installed in several ships with various kinds of propulsion, permits the angle of synchronization of the shafts to be set at any desired position from 0 deg. to 360 deg., even during running, by simply turning a small handwheel on the “adjusting differential”. It will also keep this angle constant by means of sensitive automatic control of the fuel pumps on both engines (or groups of engines), without changing the position of the fuel-control levers. &lt;br /&gt;
&lt;br /&gt;
The different applications of the &#039;&#039;&#039;De Schelde&#039;&#039;&#039; synchronizer shown in Fig. 1 are: (i) Synchronizing of propellers only, as installed in the motor liner &#039;&#039;Willem Ruys;&#039;&#039; (ii) synchronizing of crankshafts only, as installed in the single-screw motorships &#039;&#039;Carbet, Carimare&#039;&#039; and &#039;&#039;Caraibe&#039;&#039; of the French Line. A similar installation was provided for a motorship built by &#039;&#039;&#039;Kaldnes Mek. Verksted&#039;&#039;&#039;, Tønsberg, for &#039;&#039;&#039;Wilh. Wilhelmsen&#039;&#039;&#039;; and (iii) synchronizing of propellers and crankshafts. &lt;br /&gt;
[[File:1954 Syncro 1.png|alt=FIG. 2—General arrangement of hydraulic differential and control|left|thumb|250x250px|FIG. 2—General arrangement of hydraulic differential and control]]&lt;br /&gt;
This arrangement is used in the three motorships which were built for the Argentine Government, and in the new Swedish motor liner &#039;&#039;Kutigsholm.&#039;&#039; The engines in the &#039;&#039;Kungsholm&#039;&#039; consist of two &#039;&#039;&#039;Burmeister &amp;amp; Wain&#039;&#039;&#039; eight-cylinder two-stroke single-acting direct-coupled crosshead units, type 74 V TF 160, each developing 7,000 b.h.p. at 115 r.p.m. The synchronizer installed in this vessel comprises two main parts, as illustrated in Fig. 2. The first is the hydraulic differential (A) and its driving parts; and the second, the hydraulic coupling rod (B), mounted in the fuel pump control system and operated by the hydraulic differential. The hydraulic differential is an arrangement of two slides rotating one within the other. The outer slide is driven by the port engine and the inner by the starboard engine, each with a transmission ratio of 1:1. Both slides rotate in the same direction. If the starboard engine runs with the same r.p.m. as the port engine there will thus be no relative rotation between the two slides, and any relative rotation velocity of the slides is equal to the difference in r.p.m. between the two engines. Ports are milled in both inner and outer slides and, in addition two chambers are drilled in the centre of the inner slide. This divides the hydraulic differential into two parts (Fig. 3). Chamber “A” with ports I, II and III forms the oil supply side; and chamber “B” with ports IV and V forms the oil drain side.&lt;br /&gt;
[[File:1954 DES Fig 3.png|alt=FIG. 3—Cross-section showing position of ports and slides|thumb|FIG. 3—Cross-section showing position of ports and slides]]&lt;br /&gt;
There is always an open connexion through port I between chamber “A” and the oil supply line, taken from the gear pump. Similarly, chamber “B” is always connected with the oil drain pipe through the synchronizing gearbox. Ports II and V provide the oil supply and oil outlet to and from the hydraulic coupling rod on the starboard engine; ports III and IV provide these for the port engine. The hydraulic coupling rod is connected in the fuel pump control system in place of an ordinary solid rod, and consists of a cylinder, a spring-loaded piston and piston rod. The action of the oil under pressure from the hydraulic differential underneath the piston is counteracted by the spring. When the synchronizer is not working, there will be no oil pressure in the hydraulic coupling rod. The spring holds the piston against the bottom of the cylinder and the coupling rod will then act as a solid connexion. If, however, oil pressure is directed from the hydraulic differential to the coupling rod, the cylinder will be moved downwards, the position of the piston being fixed by the fuel-oil hand-control lever, reducing the capacity of the fuel pumps and slowing down the engine. The stroke of the piston in the cylinders can be adjusted from 0 to 8 mm.&lt;br /&gt;
&lt;br /&gt;
—T&#039;&#039;he Shipping World, 20th January 1954; Vol. 130, pp. 116-118.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== &#039;&#039;Welding Marine Diesel Engine Structures&#039;&#039; ==&lt;br /&gt;
In ships’ machinery the materials employed have to withstand a variety of conditions. For instance, cylinder liners have to resist corrosion and wear at elevated temperatures, so has the piston, while other parts transmit or carry varying mechanical loads. For the sliding parts and cylinder liners some form of cast iron will give best service. The liners may be of alloy iron proportioned as a good compromise between low friction loss and high wear resistance. In the past all engine frames were made in cast iron, but welded steel construction is now the most popular material for the structural parts of the engine. Fewer limitations than are imposed by foundry practice enable material sections to be proportioned more economically, and due to the better distribution of material, greater accessibility to the working parts and more streamlined flow of both scavenge air and exhaust gases are made possible. In general, considerable weight saving can be achieved due to the better properties of rolled steel. Economies&lt;br /&gt;
&lt;br /&gt;
in machining can also be expected in view of the possibility of making beds and the like in fewer sections, thus saving in the number of machine joints. Modern fabrication can now be made with a small machining allowance, so achieving a saving in time and weight of metal removed. Pre-machining of detail parts on smaller machines saves time occupied on large machines later. In the design of successful fabrications the designer must have an intimate knowledge of the shop processes and must at the outset decide which of the two assembly methods suit the shop facilities best. As all engine beds are virtually a series of broad flange or deep web girders with transverse members and flanges to take the engine columns, they can be assembled from plates and sections to the shape required; the facings, which must finally be accurately machined, can be fitted last and adjusted so that they are well within the desired machining allowance. The adjustment of these facings can be made by the amount they overlap the supporting webs or by trimming the webs if they butt up on the underside. In this method of construction the main body need only be held to within reasonable limits of accuracy, and distortion due to welding will be less important, as the facings are fitted last. This method, described in its simplest form, may include a number of sub-assemblies designed to facilitate welding and reduce the risk of major error on final assembly.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;J. A. Dorrat, The Welder, January-March 1954; Vol. 23, pp. 126-130.&#039;&#039;&lt;/div&gt;</summary>
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[[File:Fig_1_Otto_4_stroke_1876.png|right|thumb|Ottos engine]]Welcome to the &#039;&#039;&#039;Old Engines Wiki&#039;&#039;&#039; - The wiki for old engines, and history in motion, for every kind of engine. &lt;br /&gt;
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Old engines and the history of internal combustion engines are fascinating topics. We try to do our part in preserving the history of these magnificient machines and their use. &lt;br /&gt;
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== We have divided up the oldengin.es website into a few speciality sites. ==&lt;br /&gt;
First, this &#039;&#039;&#039;WIKI&#039;&#039;&#039;, that itself is divided into each country and their engine makers. Multi country engine makers are listed in the country where they were founded, or where the headquarters is.  &lt;br /&gt;
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Then we have the [https://forum.oldengin.es forum] that is our social place for discussions about engines, and engine related things. Join us, and learn someting, or even better share your knowledge with fellow engineheads. &lt;br /&gt;
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We also have a blog, that lives at blog.oldengin.es, where we the websites admins publish out &amp;quot;off topic&amp;quot; things. And a general website at www.oldengin.es that we thing would publish news about the current state of engine building, and stuff that are relevant for the community. &lt;br /&gt;
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And not least a cloud archive with the content of our library of engine related literature. &lt;br /&gt;
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We have a large archive of Workshop Manuals, Parts catalogue  for some engine manufacturers, mainly German and Swedish. (mtu, Daimler Benz, Maybach Motorenbau, Scania, and Volvo Penta, and a small collection of Detroit Diesel, Twin Disc and some other engine makers. This is available for our supporters eiter as images, or in PDF format. &lt;br /&gt;
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== Here are some of the tings we have published ==&lt;br /&gt;
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* [[:Category:Persons|Persons]] - Pages about persons we think are important to our hobby.&lt;br /&gt;
*[[:Category:Articles|Articles]] - Pages with Articles from other sources than own research. &lt;br /&gt;
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== Who are we? ==&lt;br /&gt;
oldengin.es is a domain name, (old engines) and some websites, and is owned by the people who runs [https://mtdb.no Motorteknisk Database] here in Norway. This website is for all the engine makers that dont fit into the mtdb.no platform. We will lean on the mtdb.no lists of engine for the Nordic countries. Also we run the DieselWiki that lives on wiki.cdd.no that mainly cares about Daimler, Benz, Maybach and Zeppelin derived companies and engines.   &lt;br /&gt;
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And it is a way to get some of the history of old engines archived on the internet. We are not doing this to make money, the only thing supporters contributes to is the running costs of this website, and occasional bids on ebay to buy some documentation in high demand.&lt;br /&gt;
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== Why? ==&lt;br /&gt;
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== Can i contribute? You need some help? ==&lt;br /&gt;
Yes you can, let us make you an account at this engine wiki, and you can publish your knowledge. Mail us at dieselmotor@outlook.com&lt;br /&gt;
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==Links to interesting places==&lt;br /&gt;
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https://www.industriegeschichte-ludwigsfelde.de&lt;br /&gt;
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https://themator.museum-digital.de/ausgabe/showthema.php?m_tid=2056&amp;amp;tid=2056&amp;amp;ver=standalone&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1954&amp;diff=880</id>
		<title>Engineering Abstracts 1954</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1954&amp;diff=880"/>
		<updated>2026-03-28T17:55:10Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
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[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
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= Engineering Abstracts 1954 =&lt;br /&gt;
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== Large Nine-cylinder Diesel Engine ==&lt;br /&gt;
A nine-cylinder engine designed to develop 11,200 b.h.p. at 115 r.p.m. under normal conditions at sea has recendy been completed by Burmeister and Wain. It has cylinders 740 mm. in diameter with a piston stroke of 1,600 mm., and is to be installed in a tanker under construction at the Nakskov Skibsvaerft for A.P. Moller, Copenhagen. It is the highest-powered marine engine constructed by Burmeister and Wain.&lt;br /&gt;
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The new engine is equipped with three turbochargers of the Brown-Boveri VTR-630 type, these blowers being similar to those employed in the main engines of A. P. Moller’s M.S. &#039;&#039;Dorthe Maersk&#039;&#039; and the &#039;&#039;Songkhla, Samoa&#039;&#039; and &#039;&#039;Sibonga&#039;&#039; of the East Asiatic Co. The output of the 11,200 b.h.p. engine is slightly higher than that of a corresponding 12-cylinder non-turbo-charged unit, which is about 10 feet 10 inches longer and 35 per cent heavier than the nine-cylinder turbo-charged engine. Ten nine-cylinder engines of this type are being built by Burmeister and Wain and one with 10 cylinders, for a cargo ship, at Eriksbergs Mek. Verk. developing 12,500 b.h.p. In Japan an engine has been installed in the recently completed &#039;&#039;Hanmasan Maru,&#039;&#039; a cargo ship of 10,200 tons with a service speed of 17} knots. The fuel consumption of these engines, based upon the results of similar but smaller units installed in ships now in service is expected to be 0 3341b. per b.h.p. hr., the mechanical efficiency being about 88 per cent. In normal service the mean indicated pressure is approximately 1021b. per sq. in.&lt;br /&gt;
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—&#039;&#039;The Motor Ship, March 1954; Vol. 34, p. 518.&#039;&#039;&lt;br /&gt;
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== Cas Turbine Progress ==&lt;br /&gt;
Marine auxiliary and industrial gas turbines ranging in power from 140 to 900 kW are being developed at Bedford by W. H. Allen, Sons and Co., Ltd. Of the four basic designs involved, the smallest is an all-radial-flow single-shaft unit with a rating of 200 b.h.p. (140 kW) at an air inlet temperature of 60 deg. F. (15 deg. C .); the prototype is now undergoing extensive testing and development. Designed originally at the request of the Admiralty, this small engine is intended for any duty where low fuel consumption is of less importance than such advantages as light weight, compactness, quick starting, rapid acceptance of load, and absence of cooling water. An ingenious feature is the use of a one-piece turbo-compressor rotor, with the centrifugal impeller vanes machined from one face of a forged steel disc and the centripetal turbine vanes from the other. By thus taking the familiar back-to-back arrangement of radial-flow components to its logical conclusion, the opportunity is presented of cooling the turbine by direct heat transfer across the rotor disc. The Allen designers have applied this principle so successfully that the ferritic steel disc of the prototype engine shows every sign of lasting for many thousands of running hours despite the use of inlet gas temperatures up to 800 deg. C. (1,470 deg. F.). A larger gas turbine of familiar type to the 200-b.h.p. unit has been designed, and manufacture will commence shortly. Six d.c. generator-driving versions of it have been ordered by the Alfred H olt shipping concern for auxiliary use aboard Blue Funnel liners, the rating being 350 kW at an air inlet temperature of 85 deg. F. (30 deg. C.). These sets are too large to make efficient use of a radial-flow turbine, so the single-stage centrifugal impeller is driven in each case by a two-stage axial turbine. On behalf of the Admiralty, the company is designing and constructing two interesting gas-turbo-alternators rated at 500 kW in tropical conditions. No details have yet been released for publication.&lt;br /&gt;
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—&#039;&#039;The Oil Engine and Gas Turbine, March 1954; Vol. 21, p. 436.&#039;&#039;&lt;br /&gt;
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== Centripetal Turbine tor High Specific Outputs ==&lt;br /&gt;
In 1939 the U.S. Navy Department requested bids on two 2,500-h.p. propulsion turbines for the Navy submarine chaser PC-452. The author’s Company was awarded the contract on the basis of the evaluation made by the U.S. Navy Department, which took into consideration the weight of the turbines, their overall dimensions, and their efficiency. The Company’s design study resulted in the choice of a compound turbine arrangement—this is, a high-pressure and a separate low-pressure turbine for each of the two propelling units. It also indicated that it was necessary to operate these turbines at no less than 15,000 r.p.m. if the design target (with regard to bulk, weight, and efficiency) was to be met. This high speed ruled out the axial-flow wheel for the last stage of the low-pressure turbine, because this type is incapable of passing the large volume flows at such high r.p.m., without prohibitively low efficiency. The high-specific-speed centripetal turbine came to the rescue, and was used not only in the last stage but also in the next-to-last stage of the low-pressure turbine,&lt;br /&gt;
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a sectional view of which is shown in Fig. 10. This particular application of the high-specific-speed centripetal turbine made possible the attainment of a specific weight, for the complete unit, of only slightly over 31b.-per-shaft horsepower, including the double reduction gear, turning gear, and other accessories. This specific weight is by far the lowest that has ever been achieved for a marine propelling steam turbine. The units fully met the efficiency guarantees, and their small dimensions made it possible to accommodate them easily in the confined space of the slender hull. Several different sizes of turbosuperchargers for Diesel engines have been constructed in the past four years by the author’s Company. In the course of the development of these units it has been clearly demonstrated that the high-specific-speed centripetal turbine wheel is the ideal answer for this application for the following reasons: 1. This turbine is capable of an r.p.m. sufficiently high to bring the compressor driven by it into a specific speed range where maximum compressor efficiency can be obtained. An axial-flow turbine designed for the same flow and stress conditions would have to operate at lower r.p.m., which would result in a correspondingly lower specific speed of the compressor, thus preventing the attainment of maximum possible compressor efficiency. 2. Under the particular flow and operating conditions encountered in the service of exhaust turbines for Diesel engines, distinctly higher turbine efficiency can be obtained with the centripetal turbine than is possible with the axial-flow type. 3. The efficiency of the centripetal turbine, which in itself is high, can be further increased by the recovery of kinetic energy in the turbine exhaust through the use of an exhaust diffuser in the form of a simple conical duct. 4. The centripetal turbine, owing to its low number of husky blades, is far less delicate than the axial-flow wheel and better able to cope with the severe service of Diesel-engine exhaust gas operation. In addition thereto, it is cheaper to manufacture. 5. The turbine blades and turbine rotor hub can be cooled in a simple manner, similar to the one described for the aircraft exhaust gas turbines. This reduces the metal temperatures even under the extreme conditions of Diesel-engine preturbine temperature encountered during engine overload conditions, to values which permit designing for virtually unlimited time to rupture. 6. The inertia of the centripetal wheel is lower than that of an equivalent axial-flow wheel, which results in a more rapid change of turbo-supercharger speed with a change in engine load. 7. The stationary turbine nozzles, directing the flow into the centripetal wheel, can be arranged between parallel radial walls, which makes it practicable to provide for pivoting the guide vanes to adjust the nozzle areas and angles for matching the turbo-supercharger to the engine.&lt;br /&gt;
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—&#039;&#039;R. Birmunn, Transactions of the A.S.M.E., February 1954; Vol. 76, pp. 173-187.&#039;&#039;&lt;br /&gt;
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== Motorships for South America ==&lt;br /&gt;
Canadian Vickers, Ltd., of Montreal is again delivering ships to The Flota Mercante Grancolombiana. First two of a series of four additional motorships, the &#039;&#039;Ciudad de Valencia&#039;&#039; and &#039;&#039;Ciudad de Cali,&#039;&#039; have been in service several months. The other two vessels, the &#039;&#039;Ciudad de Ibague&#039;&#039; and &#039;&#039;Ciudad de Cumana&#039;&#039; will be delivered in the forthcoming months. In accord with their building programme, Flota Mercante Grancolombiana, S.A., placed orders with Canadian Vickers, Ltd. for the construction of these four new vessels to augment their very fast cargo carrying service between the major ports of Venezuela, Colombia, Ecuador, New Orleans, New York and Montreal. Each ship is propelled by a single Nordberg six-cylinder Diesel engine, rated 4,275 b.h.p. at 160 r.p.m., direct connected to&lt;br /&gt;
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the propeller shaft. The engine has a 29in. bore by a 40in. stroke and is of the two-cycle, single-acting type with port scavenging and port exhaust. The propulsion Diesel is independently scavenged by two motor-driven blowers each of 200 h.p. rating, taking air from the engine room through a Maxim silencer and each discharging 10,000 cfm. at about 2 -41b. per sq. in. discharge pressure to a common intake manifold. This method of obtaining scavenge air results in a shorter engine, and in case of failure of one of the blowers, the engine is still capable of maintaining 70 per cent ship speed with the remaining blower. The main engine control platform is at the after end of the engine on the port side and the log desk, engine telegraph, instrument panel, alarm panel, telephone booth are all disposed conveniently around the operator and are actuated by automatic controls. They have an actual air delivery of 68 cfm. at 870 r.p.m. and are of the two-stage type, water cooled and fitted with inter and after cooler. Auxiliary power on each of the vessels is supplied by three Nordberg four-cycle, eight-cylinder inter-cooled-super-charged Diesel engines. These engines are of the single-acting, trunk piston, mechanical injection type with cylinders of 9in. bore and ll^in . stroke rated 580 h.p. at 600 r.p.m. Each drives a 400 kW. 120/240 volt, 3 phase Westinghouse generator arranged for parallel operation and capable of carrying a 25 per cent out of balance current.&lt;br /&gt;
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—&#039;&#039;D. Shearing, Diesel Progress, December 1953; Vol. 19, pp. 42-43.&#039;&#039;&lt;br /&gt;
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== Diesel-electric Tanker ==&lt;br /&gt;
The accompanying illustration shows one of the two Diesel-electric propelling motors of 1,750 h.p. at 128 r.p.m. in the 9,300-tons Soviet tanker &#039;&#039;General Asi Aslanow.&#039;&#039; The motors are supplied with direct current at 700 volts from four 700 kW. D.C. generators, each driven by a supercharged six-cylinder four-stroke cycle Diesel engine at 900 b.h.p. at 720 r.p.m. Cylinder diameter is 308 mm. and stroke is 330 mm. The pistons are of light alloy and are not liquid cooled.&lt;br /&gt;
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—S. &#039;&#039;Antonow, Schiffbautechnik, December 1953; Vol. 3, pp. 359-362.&#039;&#039;&lt;br /&gt;
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== Cas Turbined Coaster ==&lt;br /&gt;
The first merchant vessel to be equipped with propelling machinery consisting of gas turbines fed by free-piston gas generators has recently completed her sea trials. This coaster, the &#039;&#039;Cantenac,&#039;&#039; is one of two vessels of the same type ordered by the French Ministry of Merchant Marine on behalf of Worms &amp;amp; Cie., from the Chantiers et Ateliers Augustin Norm and at Le Havre, as war loss replacement. &lt;br /&gt;
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The &#039;&#039;Cantenac&#039;&#039; is a vessel of 850 tons with three holds and has her propelling machinery arranged aft. She is 185 feet in length b.p., 30 feet 6 inches moulded breadth, 14 feet 5 inches moulded depth to main deck, and has a mean draught of 13 feet 6 inches. &lt;br /&gt;
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The propelling machinery consists of two Pescara-SIGMA type GS-34 free-piston gas generators; two gas turbines connected to a reduction gear, each fed by one gas generator; and a double reduction gear connecting the turbines to a single shaft and reducing the number of revolutions to 220 r.p.m. The complete design of this vessel, both hull and engines, has been carried out by the shipbuilders. &#039;&#039;Saving in Weight.&#039;&#039; The free-piston gas generator operates on the two-stroke cycle and consists of a horizontal cylinder with two opposed pistons, each of which is directly connected to a compressor piston. The outer part of the compressor cylinder constitutes a compensating cushion. The mixture of exhaust gas and scavenge air forms the gas which is used to drive the turbine. A comparison of the weight of a gas generator installation compared with that of a corresponding Diesel installation is in favour of the former scheme. A typical four-stroke Diesel engine, developing 1,800 h.p. at 220 r.p.m., and with 40 per cent supercharge, weighs about 1261b. per h.p., whereas a gas generator installation consisting of two GS-34 generators, one turbine and reducion gear of the same power and speed, is about 891b. per h.p. The saving in weight and bulk is only one advantage. &lt;br /&gt;
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There is also flexibility of operation, avoidance of vibration, ease of maintenance and low starting air consumption. It is claimed that in all probability the free-piston gas generator unit will become the engine with the highest thermal efficiency, with a specific fuel consumption referred to the turbine shaft of less than 0-331b. per s.h.p. per hr. At the moment it is in the region of 0 391b. per s.h.p. per hr., a figure not far different from the consumption of 0-331b. per b.h.p. per hr. obtained from a supercharged two-stroke Diesel engine. Trials were run on 19th January on fuel No. 1, which corresponds to a Redwood viscosity of about 950 secs, at 100 deg. F. The unit is designed to run on both distillator and light residual fuel.&lt;br /&gt;
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The engine was run with two gas generators developing 1,200 h.p. on one trial and with one only developing 700 h.p. on another. It is understood that the tests were highly satisfactory and it was found possible to establish, in particular, the ease and speed of manoeuvrability of the propelling machinery, as well as the ease with which one fuel was substituted for another.&lt;br /&gt;
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—&#039;&#039;The Shipping World, 17th February 1954; Vol. 130, p. 213.&#039;&#039;&lt;br /&gt;
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== Free Piston Cas Generators ==&lt;br /&gt;
The Baldwin-Lima-Hamilton free piston generator development was conducted under a (U.S.) Navy Department contract to obtain a unit suitable for naval-combatant requirements. Consequently, it was designed with a view toward high specific output, reasonably low weight, and compactness, and to provide high thermal efficiency and reliability. In other words, to fulfil its purpose, it had to compete favourably with the thermal efficiency of modern Diesel engines and give the added advantages of simplicity, low initial cost, and smooth vibrationless operation. &#039;I&#039;he power plant constructed was a twin unit with two gas generators supplying gas to a single turbine and reduction gear. It is outward-compression with both direct-bounce and reverse-bounce cylinders for control. The two gas generators are synchronized to reduce pulsations of the gas to the turbine and they can be operated together or singly, as the load requirements necessitate. The principal specifications are given as follows: —-&lt;br /&gt;
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Table 2.—B-L-H Model B Gas Generator Specifications&lt;br /&gt;
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Power-cylinder bore, inches ... ... 8 ¼&lt;br /&gt;
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Compressor-cylinder bore, inches ... 23&lt;br /&gt;
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Direct-bounce-cylinder bore, inches ... 8 ¼&lt;br /&gt;
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Reverse-bounce-cylinder bore, inches... 23&lt;br /&gt;
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Piston stroke (full load), inches ... 11&lt;br /&gt;
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Cyclic frequency (maximum), cycles per min. ... ... ... ... 1,035&lt;br /&gt;
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Exhaust pressure to turbine, lb. per sq. in. gauge ... ... ... ... 90&lt;br /&gt;
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Exhaust temperature to turbine, deg. F. 1,295&lt;br /&gt;
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Gas horsepower (maximum) ... ... 885&lt;br /&gt;
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The complete power plant, after completion of its acceptance trials at the builders’ plant, was sent to the U.S. Naval Engineering&lt;br /&gt;
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Experiment Station at Annapolis, Md., in 1950, for further test and evaluation. The principal data obtained during 700 hours of test operation are presented. Fig. 11 shows the gas-generator output, based on adiabatic expansion of the gas. The output pressure to the turbine was carried to 901b. per sq. in. gauge as contrasted with 501b. per sq. in. gauge for the French SIGM A Model GS-34. Of course, the relation of horsepower output to exhaust pressure is mainly a function of the size and characteristics of the turbine used in these tests. The curve shows outputs up to 1,770 gas-horsepower with the 901b. per sq. in. gauge maximum pressure to the turbine. On later accelerated tests to determine piston-ring and cylinder-liner suitability, where more severe operating conditions were imposed without a turbine, the same output was reached with only 701b. per sq. in. gauge exhaust pressure and the same exhaust temperature. This was a result of increasing the effective orifice area because the turbine used has a smaller equivalent orifice. The gas-horsepower curve in Fig. 11 shows that the output is increasing without any decrease in rate up to the limiting exhaust temperature and pressure set by this particular design. The shaft-horsepower curve in Fig. 11 is based on the desired 85 per cent efficiency for turbine and reduction gear, as it was in the SIGMA data. T hat efficiency&lt;br /&gt;
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was not reached with the turbine used on the actual tests. However, turbines are available with peak efficiency of 85 per cent or higher. The shaft-horsepower curve is corrected for the power requirement of the auxiliary equipment which cannot be driven directly from the turbine. Thus about 1,420 s.h.p. is available from an installation with a weight and space no greater than that of current Diesel installations and less than that of other types of power plants having comparable thermal efficiency. The model now under development at B-L-H is much smaller and lighter. Fig. 12 shows the measured fuel consumption on a gas-horsepower basis and those calculated for a possible turbine efficiency of 85 per cent. The maximum thermal efficiency of 40 3 per cent at the gasifier discharge is very satisfactory and compares favourably with the SIGMA maximum of 3 8 2 per cent. This increase in thermal efficiency&lt;br /&gt;
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is to be expected in view of higher operating conditions. The correction to a shaft-horsepower basis shows a greater reduction than was made for the SIGM A design because exact information was available on the B-L-H power plant and deduction was made for all losses, including supply of auxiliary control air, cooling-water pumping, and similar power expenditures.&lt;br /&gt;
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The only deduction made for the SIGM A unit was based on turbine efficiency of 85 per cent. It is not known if the previously published data include corrections for power to auxiliary equipment. After making these corrections to a minimum shaft-horsepower basis, the thermal efficiency is still 32’3 per cent. The turbine was rated at a maximum inlet temperature of 1,350 deg. F. However, the peak pressure of 901b. per sq. in. gauge was reached with less than 1,300 deg. F. As stated before, without the turbine and with a variation in the gas pressure-to-orifice relationship, the same temperature gave as much load with only 701b. per sq. in. gauge exhaust-gas pressure.&lt;br /&gt;
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—&#039;&#039;J. J. McMullen and W. G. Payne, Transactions of the A.S.M.E., January 1954; Vol. 76, pp. 1-14.&#039;&#039;&lt;br /&gt;
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== German Medium Speed Four-stroke Engine ==&lt;br /&gt;
[[File:1954 MAN drawing.png|left|thumb|398x398px|&#039;&#039;Sectional elevation of four-stroke M.A.N. engine&#039;&#039;]]&lt;br /&gt;
A feature of German post-war shipping has been the increasing number of ships propelled by either direct-coupled or geared M.A.N. four-stroke Diesel engines. These are m anufactured with exhaust-gas pressure-charging or as normally-aspirated units, the supercharged units having the relatively conservative mean effective pressure of 9 1 kg. per sq. cm. (129 per sq. in.). It is known, of course, that the Maschinenfabrik Augsburg Nurnberg A.G. has been actively pursuing the development of the highly supercharged four-stroke engine, the results of which have been previously published. &lt;br /&gt;
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Such engines, designed for, and operating on, higher pressures, have not yet been put into commercial service, although some are now on order, but there is, nevertheless, much of interest in the current design. This is an engine with a cylinder diameter of 400 mm. and a piston stroke of 600 mm., which, as a six-cylinder unit without supercharging, will develop 785 b.h.p. at 275 r.p.m., the corresponding piston speed being 5 5 m. per sec. The engine, which is also designed for industrial duties, is built with from five to ten cylinders—with and without pressure charging. Normal supercharging amounts to about 60 per cent, corresponding to an m.e.p. of 91 kg. per sq. cm., so that a 10-cylinder engine supercharged to this extent develops about 2,100 h.p. This is the continuous rating and does not include a 10 per cent overload allowance. A feature of the design is that arrangements have been made whereby a drive can also be taken from the forward end, if desired; this is particularly advantageous in such vessels as ferries, or for fishing boats where a drive is generally required for the trawl winch or winch generator.&lt;br /&gt;
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The exhaust-gas turbo-blower is of the standard M.A.N. design with self-aligning bearings of the multi-surface type between the turbine rotor and the blower, to ensure the minimum of friction. The construction of the engine is generally simple. The welded bedplate supports the columns and the cylinder block which, for the larger engines, comprises a number of units bolted together. Cast integral with the cylinder block is the air suction manifold which supports the camshaft seating and the fuel pumps. It will be seen that the arrangement of the camshaft is such that the need for push rods is obviated.  &lt;br /&gt;
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The drive for the camshaft is by means of a 2J-in. simplex chain. W ith four-stroke engines of similar size, reversing is generally effected in three stages, the push rods being lifted from and replaced on the cams in the first and third stages; the camshaft is moved to its requisite position during the second phase. W ith this engine, however, all cams have oblique surfaces, so that it is not necessary to lift the rollers from the cams, an arrangement which enables a simplification of the reversing gear and ensures a quicker response. Owing to the excellent heat transmission properties of the aluminium alloy of which the pistons are composed, the pistons are uncooled.&lt;br /&gt;
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With 60 per cent supercharging, the temperature at the centre of the piston crown, measured by thermo-elements 6 mm. below its surface, remains below 210 deg. C. The temperature within the vicinity of the topmost piston ring is about 20 deg. lower—about 190 deg. C. at the same load—at which temperature sticking of piston rings should not be encountered. An interesting point about the pistons is that they are ground spherically from the bottom to the top, i.e. with a smaller diameter at the bottom and top than in the middle. Furthermore, the pistons are ground slightly oval in their cross-section, the degree of ovalness increasing from the bottom upwards to about the top piston ring, where the cross section gradually reverts to round form.&lt;br /&gt;
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— &#039;&#039;The Motor Ship, February 1954; Vol. 34, pp. 486-487&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Diesel Engine Synchronization ==&lt;br /&gt;
The purpose of synchronizing is to obtain a fixed relative&lt;br /&gt;
&lt;br /&gt;
position of two rotating shafts. In a marine Diesel propelled&lt;br /&gt;
&lt;br /&gt;
installation this can be of value by removing, or at least&lt;br /&gt;
&lt;br /&gt;
reducing, disturbing vibrations which may occur in consequence&lt;br /&gt;
&lt;br /&gt;
of unbalanced inertia moments of the crankshafts, or&lt;br /&gt;
&lt;br /&gt;
resulting from a disadvantageous relative position of the rotating&lt;br /&gt;
&lt;br /&gt;
propeller blades. The De Schelde synchronizer, which&lt;br /&gt;
&lt;br /&gt;
has been installed in several ships with various kinds of propulsion,&lt;br /&gt;
&lt;br /&gt;
permits the angle of synchronization of the shafts to&lt;br /&gt;
&lt;br /&gt;
be set at any desired position from 0 deg. to 360 deg., even&lt;br /&gt;
&lt;br /&gt;
during running, by simply turning a small handwheel on the&lt;br /&gt;
&lt;br /&gt;
“adjusting differential”. It will also keep this angle constant&lt;br /&gt;
&lt;br /&gt;
by means of sensitive automatic control of the fuel pumps on&lt;br /&gt;
&lt;br /&gt;
both engines (or groups of engines), without changing the&lt;br /&gt;
&lt;br /&gt;
position of the fuel-control levers. The different applications&lt;br /&gt;
&lt;br /&gt;
of the De Schelde synchronizer shown in Fig. 1 are: (i)&lt;br /&gt;
&lt;br /&gt;
Synchronizing of propellers only, as installed in the motor liner&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;Willem Ruys;&#039;&#039; (ii) synchronizing of crankshafts only, as installed&lt;br /&gt;
&lt;br /&gt;
in the single-screw motorships &#039;&#039;Carbet, Carimare&#039;&#039; and &#039;&#039;Caraibe&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
of the French Line. A similar installation was provided for a motorship built by Kaldnes Mek. Verksted, Tonsberg, for&lt;br /&gt;
&lt;br /&gt;
Wilh. Wilhelmsen; and (iii) synchronizing of propellers and&lt;br /&gt;
&lt;br /&gt;
crankshafts. This arrangement is used in the three motorships&lt;br /&gt;
&lt;br /&gt;
which were built for the Argentine Government, and in the&lt;br /&gt;
&lt;br /&gt;
new Swedish motor liner &#039;&#039;Kutigsholm.&#039;&#039; The engines in the&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;Kungsholm&#039;&#039; consist of two Burmeister and Wain eight-cylinder&lt;br /&gt;
&lt;br /&gt;
two-stroke single-acting direct-coupled crosshead units, type&lt;br /&gt;
&lt;br /&gt;
74 V TF 160, each developing 7,000 b.h.p. at 115 r.p.m. The&lt;br /&gt;
&lt;br /&gt;
synchronizer installed in this vessel comprises two main parts,&lt;br /&gt;
&lt;br /&gt;
as illustrated in Fig. 2. The first is the hydraulic differential&lt;br /&gt;
&lt;br /&gt;
(A) and its driving parts; and the second, the hydraulic coupling&lt;br /&gt;
&lt;br /&gt;
rod (B), mounted in the fuel pump control system and&lt;br /&gt;
&lt;br /&gt;
operated by the hydraulic differential. The hydraulic differential&lt;br /&gt;
&lt;br /&gt;
is an arrangement of two slides rotating one within the&lt;br /&gt;
&lt;br /&gt;
other. The outer slide is driven by the port engine and the inner by the starboard engine, each with a transmission ratio&lt;br /&gt;
&lt;br /&gt;
of 1:1. Both slides rotate in the same direction. If the starboard&lt;br /&gt;
&lt;br /&gt;
engine runs with the same r.p.m. as the port engine&lt;br /&gt;
&lt;br /&gt;
there will thus be no relative rotation between the two slides,&lt;br /&gt;
&lt;br /&gt;
and any relative rotation velocity of the slides is equal to the&lt;br /&gt;
&lt;br /&gt;
difference in r.p.m. between the two engines. Ports are milled&lt;br /&gt;
&lt;br /&gt;
in both inner and outer slides and, in addition two chambers&lt;br /&gt;
&lt;br /&gt;
are drilled in the centre of the inner slide. This divides the&lt;br /&gt;
&lt;br /&gt;
hydraulic differential into two parts (Fig. 3). Chamber “A” with ports I, II and III forms the oil supply side; and chamber&lt;br /&gt;
&lt;br /&gt;
“B” with ports IV and V forms the oil drain side. &lt;br /&gt;
&lt;br /&gt;
There is always an open connexion through port I between chamber “A” and the oil supply line, taken from the gear pump. Similarly, chamber “B” is always connected with the oil drain pipe through the synchronizing gearbox. Ports II and V provide the oil supply and oil outlet to and from the hydraulic coupling rod on the starboard engine; ports III and IV provide these for the port engine. The hydraulic coupling rod is connected in the fuel pump control system in place of an ordinary solid rod, and consists of a cylinder, a spring-loaded piston and piston rod. The action of the oil under pressure from the hydraulic differential underneath the piston is counteracted by the spring. When the synchronizer is not working, there will be no oil pressure in the hydraulic coupling rod. The spring holds the piston against the bottom of the cylinder and the coupling rod will then act as a solid connexion. If, however, oil pressure is directed from the hydraulic differential to the coupling rod, the cylinder will be moved downwards, the position of the piston being fixed by the fuel-oil hand-control lever, reducing the capacity of the fuel pumps and slowing down the engine. The stroke of the piston in the cylinders can be adjusted from 0 to 8 mm.&lt;br /&gt;
&lt;br /&gt;
—T&#039;&#039;he Shipping World, 20th January 1954; Vol. 130, pp. 116-118.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1955</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: Created page with &amp;quot;Back to the index of Engineering Abstracts  = Engineering Abstracts from 1955 =&amp;quot;&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1955 =&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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		<summary type="html">&lt;p&gt;Toro Andersen: Created page with &amp;quot;Back to the index of Engineering Abstracts  = Engineering Abstracts from 1953 =&amp;quot;&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1953 =&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1952</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: Created page with &amp;quot;Back to the index of Engineering Abstracts  = Engineering Abstracts from 1952 =&amp;quot;&lt;/p&gt;
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&lt;br /&gt;
= Engineering Abstracts from 1952 =&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1951</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: Created page with &amp;quot;Back to the index of Engineering Abstracts  = Engineering Abstracts from 1951 =&amp;quot;&lt;/p&gt;
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&lt;br /&gt;
= Engineering Abstracts from 1951 =&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1954</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;&lt;br /&gt;
[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts 1954 =&lt;br /&gt;
&lt;br /&gt;
== Large Nine-cylinder Diesel Engine ==&lt;br /&gt;
A nine-cylinder engine designed to develop 11,200 b.h.p. at 115 r.p.m. under normal conditions at sea has recendy been completed by Burmeister and Wain. It has cylinders 740 mm. in diameter with a piston stroke of 1,600 mm., and is to be installed in a tanker under construction at the Nakskov Skibsvaerft for A.P. Moller, Copenhagen. It is the highest-powered marine engine constructed by Burmeister and Wain.&lt;br /&gt;
&lt;br /&gt;
The new engine is equipped with three turbochargers of the Brown-Boveri VTR-630 type, these blowers being similar to those employed in the main engines of A. P. Moller’s M.S. &#039;&#039;Dorthe Maersk&#039;&#039; and the &#039;&#039;Songkhla, Samoa&#039;&#039; and &#039;&#039;Sibonga&#039;&#039; of the East Asiatic Co. The output of the 11,200 b.h.p. engine is slightly higher than that of a corresponding 12-cylinder non-turbo-charged unit, which is about 10 feet 10 inches longer and 35 per cent heavier than the nine-cylinder turbo-charged engine. Ten nine-cylinder engines of this type are being built by Burmeister and Wain and one with 10 cylinders, for a cargo ship, at Eriksbergs Mek. Verk. developing 12,500 b.h.p. In Japan an engine has been installed in the recently completed &#039;&#039;Hanmasan Maru,&#039;&#039; a cargo ship of 10,200 tons with a service speed of 17} knots. The fuel consumption of these engines, based upon the results of similar but smaller units installed in ships now in service is expected to be 0 3341b. per b.h.p. hr., the mechanical efficiency being about 88 per cent. In normal service the mean indicated pressure is approximately 1021b. per sq. in.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, March 1954; Vol. 34, p. 518.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cas Turbine Progress ==&lt;br /&gt;
Marine auxiliary and industrial gas turbines ranging in power from 140 to 900 kW are being developed at Bedford by W. H. Allen, Sons and Co., Ltd. Of the four basic designs involved, the smallest is an all-radial-flow single-shaft unit with a rating of 200 b.h.p. (140 kW) at an air inlet temperature of 60 deg. F. (15 deg. C .); the prototype is now undergoing extensive testing and development. Designed originally at the request of the Admiralty, this small engine is intended for any duty where low fuel consumption is of less importance than such advantages as light weight, compactness, quick starting, rapid acceptance of load, and absence of cooling water. An ingenious feature is the use of a one-piece turbo-compressor rotor, with the centrifugal impeller vanes machined from one face of a forged steel disc and the centripetal turbine vanes from the other. By thus taking the familiar back-to-back arrangement of radial-flow components to its logical conclusion, the opportunity is presented of cooling the turbine by direct heat transfer across the rotor disc. The Allen designers have applied this principle so successfully that the ferritic steel disc of the prototype engine shows every sign of lasting for many thousands of running hours despite the use of inlet gas temperatures up to 800 deg. C. (1,470 deg. F.). A larger gas turbine of familiar type to the 200-b.h.p. unit has been designed, and manufacture will commence shortly. Six d.c. generator-driving versions of it have been ordered by the Alfred H olt shipping concern for auxiliary use aboard Blue Funnel liners, the rating being 350 kW at an air inlet temperature of 85 deg. F. (30 deg. C.). These sets are too large to make efficient use of a radial-flow turbine, so the single-stage centrifugal impeller is driven in each case by a two-stage axial turbine. On behalf of the Admiralty, the company is designing and constructing two interesting gas-turbo-alternators rated at 500 kW in tropical conditions. No details have yet been released for publication.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Oil Engine and Gas Turbine, March 1954; Vol. 21, p. 436.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Centripetal Turbine tor High Specific Outputs ==&lt;br /&gt;
In 1939 the U.S. Navy Department requested bids on two 2,500-h.p. propulsion turbines for the Navy submarine chaser PC-452. The author’s Company was awarded the contract on the basis of the evaluation made by the U.S. Navy Department, which took into consideration the weight of the turbines, their overall dimensions, and their efficiency. The Company’s design study resulted in the choice of a compound turbine arrangement—this is, a high-pressure and a separate low-pressure turbine for each of the two propelling units. It also indicated that it was necessary to operate these turbines at no less than 15,000 r.p.m. if the design target (with regard to bulk, weight, and efficiency) was to be met. This high speed ruled out the axial-flow wheel for the last stage of the low-pressure turbine, because this type is incapable of passing the large volume flows at such high r.p.m., without prohibitively low efficiency. The high-specific-speed centripetal turbine came to the rescue, and was used not only in the last stage but also in the next-to-last stage of the low-pressure turbine,&lt;br /&gt;
&lt;br /&gt;
a sectional view of which is shown in Fig. 10. This particular application of the high-specific-speed centripetal turbine made possible the attainment of a specific weight, for the complete unit, of only slightly over 31b.-per-shaft horsepower, including the double reduction gear, turning gear, and other accessories. This specific weight is by far the lowest that has ever been achieved for a marine propelling steam turbine. The units fully met the efficiency guarantees, and their small dimensions made it possible to accommodate them easily in the confined space of the slender hull. Several different sizes of turbosuperchargers for Diesel engines have been constructed in the past four years by the author’s Company. In the course of the development of these units it has been clearly demonstrated that the high-specific-speed centripetal turbine wheel is the ideal answer for this application for the following reasons: 1. This turbine is capable of an r.p.m. sufficiently high to bring the compressor driven by it into a specific speed range where maximum compressor efficiency can be obtained. An axial-flow turbine designed for the same flow and stress conditions would have to operate at lower r.p.m., which would result in a correspondingly lower specific speed of the compressor, thus preventing the attainment of maximum possible compressor efficiency. 2. Under the particular flow and operating conditions encountered in the service of exhaust turbines for Diesel engines, distinctly higher turbine efficiency can be obtained with the centripetal turbine than is possible with the axial-flow type. 3. The efficiency of the centripetal turbine, which in itself is high, can be further increased by the recovery of kinetic energy in the turbine exhaust through the use of an exhaust diffuser in the form of a simple conical duct. 4. The centripetal turbine, owing to its low number of husky blades, is far less delicate than the axial-flow wheel and better able to cope with the severe service of Diesel-engine exhaust gas operation. In addition thereto, it is cheaper to manufacture. 5. The turbine blades and turbine rotor hub can be cooled in a simple manner, similar to the one described for the aircraft exhaust gas turbines. This reduces the metal temperatures even under the extreme conditions of Diesel-engine preturbine temperature encountered during engine overload conditions, to values which permit designing for virtually unlimited time to rupture. 6. The inertia of the centripetal wheel is lower than that of an equivalent axial-flow wheel, which results in a more rapid change of turbo-supercharger speed with a change in engine load. 7. The stationary turbine nozzles, directing the flow into the centripetal wheel, can be arranged between parallel radial walls, which makes it practicable to provide for pivoting the guide vanes to adjust the nozzle areas and angles for matching the turbo-supercharger to the engine.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;R. Birmunn, Transactions of the A.S.M.E., February 1954; Vol. 76, pp. 173-187.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Motorships for South America ==&lt;br /&gt;
Canadian Vickers, Ltd., of Montreal is again delivering ships to The Flota Mercante Grancolombiana. First two of a series of four additional motorships, the &#039;&#039;Ciudad de Valencia&#039;&#039; and &#039;&#039;Ciudad de Cali,&#039;&#039; have been in service several months. The other two vessels, the &#039;&#039;Ciudad de Ibague&#039;&#039; and &#039;&#039;Ciudad de Cumana&#039;&#039; will be delivered in the forthcoming months. In accord with their building programme, Flota Mercante Grancolombiana, S.A., placed orders with Canadian Vickers, Ltd. for the construction of these four new vessels to augment their very fast cargo carrying service between the major ports of Venezuela, Colombia, Ecuador, New Orleans, New York and Montreal. Each ship is propelled by a single Nordberg six-cylinder Diesel engine, rated 4,275 b.h.p. at 160 r.p.m., direct connected to&lt;br /&gt;
&lt;br /&gt;
the propeller shaft. The engine has a 29in. bore by a 40in. stroke and is of the two-cycle, single-acting type with port scavenging and port exhaust. The propulsion Diesel is independently scavenged by two motor-driven blowers each of 200 h.p. rating, taking air from the engine room through a Maxim silencer and each discharging 10,000 cfm. at about 2 -41b. per sq. in. discharge pressure to a common intake manifold. This method of obtaining scavenge air results in a shorter engine, and in case of failure of one of the blowers, the engine is still capable of maintaining 70 per cent ship speed with the remaining blower. The main engine control platform is at the after end of the engine on the port side and the log desk, engine telegraph, instrument panel, alarm panel, telephone booth are all disposed conveniently around the operator and are actuated by automatic controls. They have an actual air delivery of 68 cfm. at 870 r.p.m. and are of the two-stage type, water cooled and fitted with inter and after cooler. Auxiliary power on each of the vessels is supplied by three Nordberg four-cycle, eight-cylinder inter-cooled-super-charged Diesel engines. These engines are of the single-acting, trunk piston, mechanical injection type with cylinders of 9in. bore and ll^in . stroke rated 580 h.p. at 600 r.p.m. Each drives a 400 kW. 120/240 volt, 3 phase Westinghouse generator arranged for parallel operation and capable of carrying a 25 per cent out of balance current.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;D. Shearing, Diesel Progress, December 1953; Vol. 19, pp. 42-43.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Diesel-electric Tanker ==&lt;br /&gt;
The accompanying illustration shows one of the two Diesel-electric propelling motors of 1,750 h.p. at 128 r.p.m. in the 9,300-tons Soviet tanker &#039;&#039;General Asi Aslanow.&#039;&#039; The motors are supplied with direct current at 700 volts from four 700 kW. D.C. generators, each driven by a supercharged six-cylinder four-stroke cycle Diesel engine at 900 b.h.p. at 720 r.p.m. Cylinder diameter is 308 mm. and stroke is 330 mm. The pistons are of light alloy and are not liquid cooled.&lt;br /&gt;
&lt;br /&gt;
—S. &#039;&#039;Antonow, Schiffbautechnik, December 1953; Vol. 3, pp. 359-362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cas Turbined Coaster ==&lt;br /&gt;
The first merchant vessel to be equipped with propelling machinery consisting of gas turbines fed by free-piston gas generators has recently completed her sea trials. This coaster, the &#039;&#039;Cantenac,&#039;&#039; is one of two vessels of the same type ordered by the French Ministry of Merchant Marine on behalf of Worms &amp;amp; Cie., from the Chantiers et Ateliers Augustin Norm and at Le Havre, as war loss replacement. &lt;br /&gt;
&lt;br /&gt;
The &#039;&#039;Cantenac&#039;&#039; is a vessel of 850 tons with three holds and has her propelling machinery arranged aft. She is 185 feet in length b.p., 30 feet 6 inches moulded breadth, 14 feet 5 inches moulded depth to main deck, and has a mean draught of 13 feet 6 inches. &lt;br /&gt;
&lt;br /&gt;
The propelling machinery consists of two Pescara-SIGMA type GS-34 free-piston gas generators; two gas turbines connected to a reduction gear, each fed by one gas generator; and a double reduction gear connecting the turbines to a single shaft and reducing the number of revolutions to 220 r.p.m. The complete design of this vessel, both hull and engines, has been carried out by the shipbuilders. &#039;&#039;Saving in Weight.&#039;&#039; The free-piston gas generator operates on the two-stroke cycle and consists of a horizontal cylinder with two opposed pistons, each of which is directly connected to a compressor piston. The outer part of the compressor cylinder constitutes a compensating cushion. The mixture of exhaust gas and scavenge air forms the gas which is used to drive the turbine. A comparison of the weight of a gas generator installation compared with that of a corresponding Diesel installation is in favour of the former scheme. A typical four-stroke Diesel engine, developing 1,800 h.p. at 220 r.p.m., and with 40 per cent supercharge, weighs about 1261b. per h.p., whereas a gas generator installation consisting of two GS-34 generators, one turbine and reducion gear of the same power and speed, is about 891b. per h.p. The saving in weight and bulk is only one advantage. &lt;br /&gt;
&lt;br /&gt;
There is also flexibility of operation, avoidance of vibration, ease of maintenance and low starting air consumption. It is claimed that in all probability the free-piston gas generator unit will become the engine with the highest thermal efficiency, with a specific fuel consumption referred to the turbine shaft of less than 0-331b. per s.h.p. per hr. At the moment it is in the region of 0 391b. per s.h.p. per hr., a figure not far different from the consumption of 0-331b. per b.h.p. per hr. obtained from a supercharged two-stroke Diesel engine. Trials were run on 19th January on fuel No. 1, which corresponds to a Redwood viscosity of about 950 secs, at 100 deg. F. The unit is designed to run on both distillator and light residual fuel.&lt;br /&gt;
&lt;br /&gt;
The engine was run with two gas generators developing 1,200 h.p. on one trial and with one only developing 700 h.p. on another. It is understood that the tests were highly satisfactory and it was found possible to establish, in particular, the ease and speed of manoeuvrability of the propelling machinery, as well as the ease with which one fuel was substituted for another.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 17th February 1954; Vol. 130, p. 213.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Free Piston Cas Generators ==&lt;br /&gt;
The Baldwin-Lima-Hamilton free piston generator development was conducted under a (U.S.) Navy Department contract to obtain a unit suitable for naval-combatant requirements. Consequently, it was designed with a view toward high specific output, reasonably low weight, and compactness, and to provide high thermal efficiency and reliability. In other words, to fulfil its purpose, it had to compete favourably with the thermal efficiency of modern Diesel engines and give the added advantages of simplicity, low initial cost, and smooth vibrationless operation. &#039;I&#039;he power plant constructed was a twin unit with two gas generators supplying gas to a single turbine and reduction gear. It is outward-compression with both direct-bounce and reverse-bounce cylinders for control. The two gas generators are synchronized to reduce pulsations of the gas to the turbine and they can be operated together or singly, as the load requirements necessitate. The principal specifications are given as follows: —-&lt;br /&gt;
&lt;br /&gt;
Table 2.—B-L-H Model B Gas Generator Specifications&lt;br /&gt;
&lt;br /&gt;
Power-cylinder bore, inches ... ... 8 ¼&lt;br /&gt;
&lt;br /&gt;
Compressor-cylinder bore, inches ... 23&lt;br /&gt;
&lt;br /&gt;
Direct-bounce-cylinder bore, inches ... 8 ¼&lt;br /&gt;
&lt;br /&gt;
Reverse-bounce-cylinder bore, inches... 23&lt;br /&gt;
&lt;br /&gt;
Piston stroke (full load), inches ... 11&lt;br /&gt;
&lt;br /&gt;
Cyclic frequency (maximum), cycles per min. ... ... ... ... 1,035&lt;br /&gt;
&lt;br /&gt;
Exhaust pressure to turbine, lb. per sq. in. gauge ... ... ... ... 90&lt;br /&gt;
&lt;br /&gt;
Exhaust temperature to turbine, deg. F. 1,295&lt;br /&gt;
&lt;br /&gt;
Gas horsepower (maximum) ... ... 885&lt;br /&gt;
&lt;br /&gt;
The complete power plant, after completion of its acceptance trials at the builders’ plant, was sent to the U.S. Naval Engineering&lt;br /&gt;
&lt;br /&gt;
Experiment Station at Annapolis, Md., in 1950, for further test and evaluation. The principal data obtained during 700 hours of test operation are presented. Fig. 11 shows the gas-generator output, based on adiabatic expansion of the gas. The output pressure to the turbine was carried to 901b. per sq. in. gauge as contrasted with 501b. per sq. in. gauge for the French SIGM A Model GS-34. Of course, the relation of horsepower output to exhaust pressure is mainly a function of the size and characteristics of the turbine used in these tests. The curve shows outputs up to 1,770 gas-horsepower with the 901b. per sq. in. gauge maximum pressure to the turbine. On later accelerated tests to determine piston-ring and cylinder-liner suitability, where more severe operating conditions were imposed without a turbine, the same output was reached with only 701b. per sq. in. gauge exhaust pressure and the same exhaust temperature. This was a result of increasing the effective orifice area because the turbine used has a smaller equivalent orifice. The gas-horsepower curve in Fig. 11 shows that the output is increasing without any decrease in rate up to the limiting exhaust temperature and pressure set by this particular design. The shaft-horsepower curve in Fig. 11 is based on the desired 85 per cent efficiency for turbine and reduction gear, as it was in the SIGMA data. T hat efficiency&lt;br /&gt;
&lt;br /&gt;
was not reached with the turbine used on the actual tests. However, turbines are available with peak efficiency of 85 per cent or higher. The shaft-horsepower curve is corrected for the power requirement of the auxiliary equipment which cannot be driven directly from the turbine. Thus about 1,420 s.h.p. is available from an installation with a weight and space no greater than that of current Diesel installations and less than that of other types of power plants having comparable thermal efficiency. The model now under development at B-L-H is much smaller and lighter. Fig. 12 shows the measured fuel consumption on a gas-horsepower basis and those calculated for a possible turbine efficiency of 85 per cent. The maximum thermal efficiency of 40 3 per cent at the gasifier discharge is very satisfactory and compares favourably with the SIGMA maximum of 3 8 2 per cent. This increase in thermal efficiency&lt;br /&gt;
&lt;br /&gt;
is to be expected in view of higher operating conditions. The correction to a shaft-horsepower basis shows a greater reduction than was made for the SIGM A design because exact information was available on the B-L-H power plant and deduction was made for all losses, including supply of auxiliary control air, cooling-water pumping, and similar power expenditures.&lt;br /&gt;
&lt;br /&gt;
The only deduction made for the SIGM A unit was based on turbine efficiency of 85 per cent. It is not known if the previously published data include corrections for power to auxiliary equipment. After making these corrections to a minimum shaft-horsepower basis, the thermal efficiency is still 32’3 per cent. The turbine was rated at a maximum inlet temperature of 1,350 deg. F. However, the peak pressure of 901b. per sq. in. gauge was reached with less than 1,300 deg. F. As stated before, without the turbine and with a variation in the gas pressure-to-orifice relationship, the same temperature gave as much load with only 701b. per sq. in. gauge exhaust-gas pressure.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;J. J. McMullen and W. G. Payne, Transactions of the A.S.M.E., January 1954; Vol. 76, pp. 1-14.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Medium Speed Four-stroke Engine ==&lt;br /&gt;
[[File:1954 MAN drawing.png|left|thumb|398x398px|&#039;&#039;Sectional elevation of four-stroke M.A.N. engine&#039;&#039;]]&lt;br /&gt;
A feature of German post-war shipping has been the increasing number of ships propelled by either direct-coupled or geared M.A.N. four-stroke Diesel engines. These are m anufactured with exhaust-gas pressure-charging or as normally-aspirated units, the supercharged units having the relatively conservative mean effective pressure of 9 1 kg. per sq. cm. (129 per sq. in.). It is known, of course, that the Maschinenfabrik Augsburg Nurnberg A.G. has been actively pursuing the development of the highly supercharged four-stroke engine, the results of which have been previously published. &lt;br /&gt;
&lt;br /&gt;
Such engines, designed for, and operating on, higher pressures, have not yet been put into commercial service, although some are now on order, but there is, nevertheless, much of interest in the current design. This is an engine with a cylinder diameter of 400 mm. and a piston stroke of 600 mm., which, as a six-cylinder unit without supercharging, will develop 785 b.h.p. at 275 r.p.m., the corresponding piston speed being 5 5 m. per sec. The engine, which is also designed for industrial duties, is built with from five to ten cylinders—with and without pressure charging. Normal supercharging amounts to about 60 per cent, corresponding to an m.e.p. of 91 kg. per sq. cm., so that a 10-cylinder engine supercharged to this extent develops about 2,100 h.p. This is the continuous rating and does not include a 10 per cent overload allowance. A feature of the design is that arrangements have been made whereby a drive can also be taken from the forward end, if desired; this is particularly advantageous in such vessels as ferries, or for fishing boats where a drive is generally required for the trawl winch or winch generator.&lt;br /&gt;
&lt;br /&gt;
The exhaust-gas turbo-blower is of the standard M.A.N. design with self-aligning bearings of the multi-surface type between the turbine rotor and the blower, to ensure the minimum of friction. The construction of the engine is generally simple. The welded bedplate supports the columns and the cylinder block which, for the larger engines, comprises a number of units bolted together. Cast integral with the cylinder block is the air suction manifold which supports the camshaft seating and the fuel pumps. It will be seen that the arrangement of the camshaft is such that the need for push rods is obviated.  &lt;br /&gt;
&lt;br /&gt;
The drive for the camshaft is by means of a 2J-in. simplex chain. W ith four-stroke engines of similar size, reversing is generally effected in three stages, the push rods being lifted from and replaced on the cams in the first and third stages; the camshaft is moved to its requisite position during the second phase. W ith this engine, however, all cams have oblique surfaces, so that it is not necessary to lift the rollers from the cams, an arrangement which enables a simplification of the reversing gear and ensures a quicker response. Owing to the excellent heat transmission properties of the aluminium alloy of which the pistons are composed, the pistons are uncooled.&lt;br /&gt;
&lt;br /&gt;
With 60 per cent supercharging, the temperature at the centre of the piston crown, measured by thermo-elements 6 mm. below its surface, remains below 210 deg. C. The temperature within the vicinity of the topmost piston ring is about 20 deg. lower—about 190 deg. C. at the same load—at which temperature sticking of piston rings should not be encountered. An interesting point about the pistons is that they are ground spherically from the bottom to the top, i.e. with a smaller diameter at the bottom and top than in the middle. Furthermore, the pistons are ground slightly oval in their cross-section, the degree of ovalness increasing from the bottom upwards to about the top piston ring, where the cross section gradually reverts to round form.&lt;br /&gt;
&lt;br /&gt;
— &#039;&#039;The Motor Ship, February 1954; Vol. 34, pp. 486-487&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=File:1954_MAN_drawing.png&amp;diff=874</id>
		<title>File:1954 MAN drawing.png</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=File:1954_MAN_drawing.png&amp;diff=874"/>
		<updated>2026-03-28T17:47:53Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;Drawing of a MAN 1954 model&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=873</id>
		<title>Engineering Abstracts 1959</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=873"/>
		<updated>2026-03-28T16:09:14Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: /* River Tankers with Voith Schneider Propulsion */&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at &#039;&#039;&#039;Gotaverken&#039;&#039;&#039; Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. &lt;br /&gt;
&lt;br /&gt;
The project prepared by &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. &lt;br /&gt;
&lt;br /&gt;
She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. &#039;&#039;&#039;Pielstick&#039;&#039;&#039; machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. &#039;&#039;&#039;SEMT-Pielstick&#039;&#039;&#039; engines are coupled to two shafts through an &#039;&#039;&#039;ASEA&#039;&#039;&#039; electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. &lt;br /&gt;
&lt;br /&gt;
To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). &lt;br /&gt;
&lt;br /&gt;
They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. &lt;br /&gt;
&lt;br /&gt;
They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. &lt;br /&gt;
&lt;br /&gt;
The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a &#039;&#039;&#039;British Polar Diesel&#039;&#039;&#039; engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. &lt;br /&gt;
&lt;br /&gt;
The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. &#039;&#039;&#039;Westinghouse&#039;&#039;&#039; type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. &lt;br /&gt;
&lt;br /&gt;
This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. &lt;br /&gt;
&lt;br /&gt;
The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. &lt;br /&gt;
&lt;br /&gt;
While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems.  &lt;br /&gt;
&lt;br /&gt;
Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber.  &lt;br /&gt;
&lt;br /&gt;
A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
The telescope valve engine is an improved four-stroke cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are also favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. &lt;br /&gt;
&lt;br /&gt;
Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. &lt;br /&gt;
&lt;br /&gt;
To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. &lt;br /&gt;
&lt;br /&gt;
The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. &lt;br /&gt;
&lt;br /&gt;
The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. &lt;br /&gt;
&lt;br /&gt;
For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. &lt;br /&gt;
&lt;br /&gt;
From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead &#039;&#039;&#039;Bolnes&#039;&#039;&#039; engine with a bore of 190 mm. This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. &lt;br /&gt;
&lt;br /&gt;
As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. &lt;br /&gt;
&lt;br /&gt;
The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The &#039;&#039;&#039;Stork&#039;&#039;&#039; marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. &lt;br /&gt;
&lt;br /&gt;
The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. &lt;br /&gt;
&lt;br /&gt;
The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. &lt;br /&gt;
&lt;br /&gt;
The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. &lt;br /&gt;
&lt;br /&gt;
The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. &lt;br /&gt;
&lt;br /&gt;
As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. &lt;br /&gt;
&lt;br /&gt;
The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder &#039;&#039;&#039;Doxford&#039;&#039;&#039; type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd.  &lt;br /&gt;
&lt;br /&gt;
The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; main engines. The installation, which has been built by &#039;&#039;&#039;Stothert and Pitt&#039;&#039;&#039;, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by &#039;&#039;&#039;Renold’s&#039;&#039;&#039; chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency.  &lt;br /&gt;
&lt;br /&gt;
There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr.  &lt;br /&gt;
&lt;br /&gt;
The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure.  &lt;br /&gt;
&lt;br /&gt;
Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “&#039;&#039;&#039;Bolnes&#039;&#039;&#039;” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the &#039;&#039;&#039;Graviner Manufacturing&#039;&#039;&#039; Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. &#039;&#039;&#039;Ruston and Hornsby&#039;&#039;&#039;, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of 10in., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the boat which drives a screw propeller so mounted on a support that the axis of the propeller is movable relative to the fore and aft axis of the boat for steering, the support itself being pivotable about a horizontal axis to lift the screw propeller clear of the water. In Fig. 1 the engine shaft extends in a fore and aft direction into the lower part of the chain case (36) to carry a chain sprocket (44). The shaft (29) which extends through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member lies within the chain case in the same plane as the sprocket (44) being adjacent with the upper end of the chain case. A sprocket chain (46) runs over the two sprockets. Two arms (47), pivotally mounted in the chain case and extending downwardly from their pivotal mountings, carry at their free ends sprockets (48) which engage the chain (46) inside its loop between the sprockets (44 and 45), the arms (47) being acted on by springs (49). The latter tend to urge the arms upwardly and outwardly. The upward and outward movement of the arms (47) is limited by stops (50) so as to ensure that they move through equal distances. It will be apparent that the propeller (26) can be lifted out of the water by rocking the L-shaped member (15, 16) rearwardly and upwardly about the trunnions (17) and such rocking movement will cause the sprocket (45) to swing downwardly and rearwardly. The upper part of the chain loop will tend to move downwardly with the sprocket (45) introducing slack in the chain (46) which will be taken up by upward movement of the idler sprockets (48). Ultimately, when the upper part of the chain (46) extends in a substantially straight line between the sprockets (48), as indidated in dotted lines in Fig. 2, the sprocket (45) will move away from the chain and the driving connexion between the engine and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Development of Borsig-Fiat Engine ==&lt;br /&gt;
[[File:1959 Borsig Fiat Fig 2.png|alt=Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C. |left|thumb|380x380px|&#039;&#039;Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C.&#039;&#039;]]&lt;br /&gt;
The Buries Markes motor ship &#039;&#039;La Selva,&#039;&#039; is equipped with a &#039;&#039;&#039;Borsig-Fiat&#039;&#039;&#039; engine with six cylinders, 680 mm. in diameter, having a piston stroke of 1,200 mm. and a normal output of 4,750 b.h.p. at 130 r.p.m. The fuel used is Bunker C, up to 3,500 sec. Redwood I at 100 deg. F. During the shop trials, an output of 3,550 b.h.p. was attained at 118 r.p.m., with a mean effective pressure of 5-2 kg./sq. cm., when the turbochargers were out of action and air was drawn in directly from the engine room to the piston scavenge pumps. &lt;br /&gt;
&lt;br /&gt;
This output corresponds to 75 per cent of the full load power according to the propeller curve, whilst the m.e.p. value is similar to that with the unsupercharged engine. The exhaust temperature before the turbines did not exceed the normal value of 320 deg. C. and the change over from non-turbocharged operation to turbocharging could be made in a very short time. &lt;br /&gt;
[[File:1959 Borsig Fiat Fig 3.png|alt=Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. |thumb|250x250px|Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. ]]&lt;br /&gt;
Thus, all that was needed to attain 75 per cent output without turbocharging was to lock the turbocharger rotors and remove two manhole covers. Further developments have been made in this model, the speed being raised to 140 r.p.m. and the mean pressure to 6-86 kg./sq. cm. Under these conditions the engine has an output of 5,580 b.h.p. The maximum output of 6,300 b.h.p. or 1,050 b.h.p. per cylinder at about 146 r.p.m. is attained with an m.e.p. of 7-4 kg./sq. cm., corresponding to a mean piston speed of 5-8 m./sec. This is the load which the engine is capable of delivering on the test bed and sea trials for a period of three hours. The rated cylinder output of 930 b.h.p. at 140 r.p.m. with an m.e.p. of 6-86 kg./sq. cm., is that for which the engine is designed on the basis of the prevailing rules of the classification societies. The recommended output for continuous service is 80 per cent to 95 per cent of the rated output, according to the actual service conditions, namely, length and severity of the voyages, the frequency and duration of harbour stops, the ambient conditions of the engine room, the quality of fuel and the state of maintenance of the engine. The Borsig-Fiat engine is exhaust turbocharged on the constant pressure series principle, the two exhaust turbochargers being of the &#039;&#039;&#039;BBC&#039;&#039;&#039;.VTR 500 type with voluted gas intakes. They are arranged ahead of the crosshead driven double acting piston scavenge pumps, the total volume of which is about 1-3 times that of the power cylinders. During the trials at the works, it was ascertained that the proportion of the compression work of the turbochargers increases with increasing engine load, while the proportion of the compression work of the engine driven scavenge pumps decreases. This characteristic is desirable from the standpoint of engine efficiency. At full load the turbochargers provide about 75 per cent of the total work required for the compression of the charging and scavenge air. Upon starting, when accelerating and in the low speed range, the piston scavenge pumps provide most of the air supply because the turbochargers do not then deliver their full capacity. In the lower speed ranges, as well as at higher speeds, the engine is readily responsive, with a smoke free exhaust. Detailed results of the tests of the 4,750-b.h.p. engine in the &#039;&#039;La Selva&#039;&#039; are shown in Fig. 2, whilst in Fig. 3 the results achieved with the engine after the further development are indicated. They show a total increase of 17-5 per cent, from 4,750 to 5,580 b.h.p., with a simultaneous rise of 130 r.p.m. to 140 r.p.m., or 7-8 per cent and a boost in b.m.e.p. from 6-3 kg. per sq. cm. to &#039;&#039;6-86&#039;&#039; kg. per sq. cm., or 9 per cent. The exhaust temperatures of the stepped-up 5,580-b.h.p. engine are 10 per cent higher whilst the charging air temperature after the blowers and before the scavenge ports, as well as the air pressure before the latter, have fallen slightly in spite of the increased boost. The ignition pressure of 65 kg. per sq. cm. when running on Diesel oil (60 kg. per sq. cm. when burning heavy fuel) remains the same. These improvements were rendered possible through higher efficiencies of the turbochargers, and improved adaptation of these blowers to the engine’s operating conditions. This also explains, for the most part, the reduction in specific fuel consumption from 164 gr. per b.h.p. per hr. to 156 gr. per b.h.p. per hr. or 4-7 per cent.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, May 1959; Vol. 40, pp. 86-87.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 24,000-b.H.p. Diesel Plant for Supertanker ==&lt;br /&gt;
[[File:1959 MAN 24000 BHP Diesel plant.png|alt=(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.|thumb|&#039;&#039;(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&#039;&#039;]]&lt;br /&gt;
In conjunction with a shipbuilding concern and a shipping company, the &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. have put forward plans for the propulsion machinery of 24,000 b.h.p. for a supertanker. The four engines are of standard &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. two-stroke type with 25 per cent turbocharging, the cylinders having a diameter of 570 mm. and a piston stroke of 800 mm. The speed is 225 r.p.m. The installation comprises two engines each of 7,300 b.h.p. driving a single shaft through hydraulic or electromagnetic couplings, and two engines of 6,000 b.h.p. in the wings and on a platform above the engine room floor, each driving an alternator supplying current to two 5,400-b.h.p. electric motors driving the same shaft through gearing. &lt;br /&gt;
&lt;br /&gt;
The total service output is 24,000 b.h.p. Current for the auxiliaries and for other ship requirements at sea is taken from the Diesel alternators so that no other Diesel generating plant is needed when under way. The four vertical cargo pumps are electrically driven, the electric motors being installed in the engine room. There are two Diesel generating sets for harbour and emergency duties and one gas turbine driven generator. The plant is installed in an engine room of the same size as that required for steam turbine and boiler plant. The fuel consumption is not as favourable as with the slower running, direct coupled units, the additional expenditure being about 10 gr./b.h.p.-hr., but it is considered that the saving compared with steam turbine plant is so great that this factor is not of importance.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 51.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Torque Transfer Coupling ==&lt;br /&gt;
[[File:1959 The Metalastik torque transfer coupling.png|alt=The Metalastik torque transfer coupling|left|thumb|&#039;&#039;(1959) The Metalastik torque transfer coupling&#039;&#039;]]&lt;br /&gt;
An interesting feature of the new range of Ruston high pressure turbocharged four-stroke engines is the new type flexible coupling with which they are fitted. These torque transfer couplings, developed by &#039;&#039;&#039;Metalastik&#039;&#039;&#039;, Ltd., are designed expressly to provide an effective and economical solution to the problem of resonant torsional vibration and the serious consequencies arising from it in marine and other installations. &lt;br /&gt;
&lt;br /&gt;
The Metalastik coupling is said to provide initially a very low stiffness with a much higher value for a predetermined torque. The ratio of initial and final stiffness can be varied as required, this being enabled by the fact that for low torques, rubber, loaded in torsional shear, is employed, while for higher torques separate rubber buffers, loaded in compression, provide the greater degree of stiffness required. There is a rather rapid change from low to high stiffness but the characteristics of the coupling can be modified to give a more gradual charge. In addition to its capacity to damp torsional vibrations the coupling is stated to be able to accommodate some malalignment. Basically the coupling consists of two sets of three rocker arms. These are connected at their extremities by means of special shackle pins. Each arm pivots centrally on a Metalastik bush. Rubber-bonded buffers are bolted to flats formed on three of the rocker arms. These come into contact with flats on the other set of rockers when a certain torque has been reached and the initial clearance has been taken up. One set of rockers is connected by three tapered pins to the flywheel and the other set by three pins to the gearbox flange, the inner sleeves of the centre pivot bushes being keyed to the pins.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 35.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Fuel Problems in Merchant Ships ==&lt;br /&gt;
The situation has developed where marine propulsion systems can only be competitive if they are capable of using the residual fuel oil which is marketed normally as Bunker C Grade. The nature of this oil is examined, the increases which have occurred in recent years in vanadium and sulphur content being noted. The influence of shipboard storage practice, with particular reference to sludge formation, is discussed; there are remarks on the reduced likelihood of salt water contamination. The main problems encountered in boilers are considered.&lt;br /&gt;
&lt;br /&gt;
Damage to brickwork is more a matter of spalling than of slag erosion. It is suggested that the significance of vanadium may have been overrated in the problem of bonded ash deposits in conventional marine boilers. The detrimental effect on boiler efficiency of the difficulties arising from the air heater corrosion and blocking is emphasized. Cylinder wear and sticking piston rings are among the difficulties encountered when burning residual fuel oil in large marine Diesel engines. The development of gas turbines for marine use has given rise to much work during the past ten years on the problems of ash fouling and corrosion. Some observations are made on the removal of sodium from the fuel by a water washing process incorporated into the fuel system.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. McClimont, Journal of the Institute of Fuel, May 1959; Vol. 32, pp. 225-231.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion of Ships at Sea ==&lt;br /&gt;
A general consideration of screw propulsion of ships at sea leads the author to a new approach to the analysis of seagoing performance, which is regarded as the result of interactions of the relevant characteristics of engine, propeller and hull. A discussion on the torque characteristics of reciprocating engines and turbines is followed by a consideration of propeller action as influenced by immersion and by its movements in a seaway. &lt;br /&gt;
&lt;br /&gt;
When the propeller torque and thrust characteristics are also accepted as variables, a simple analysis of known records for the &#039;&#039;Simon Bolivar,&#039;&#039; the &#039;&#039;Lubumbashi,&#039;&#039; the &#039;&#039;Tervate&#039;&#039; and the &#039;&#039;Nissei Maru&#039;&#039; shows that the data can be divided into one group with the propeller apparently unaffected by ship movements and waves, and another with the propeller so affected. The still water type of results allows some new conclusions to be drawn regarding wake, propeller characteristics, and the effect of small propeller immersions, which are also, in part, valid for model test conditions. &lt;br /&gt;
&lt;br /&gt;
The results affected by waves, etc., when combined with engine characteristics, show a typical difference between reciprocating engine drive and turbine drive at sea. A few general remarks on the results are concluded by a note on the possible use of the propulsion analysis in further investigation of ship resistance and movements in waves.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;J. Oervig, Norwegian Univ. Techn. Ship Model Tank Report No. 58, 1958. Journal, The British Shipbuilding Research Association, March 1959; Vol. 14, Abstract No. 15,070.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== New W erkspoor Engine for Coasters ==&lt;br /&gt;
The new design of Werkspoor uniflow scavenged, trunk piston engine, is to be installed in a new ship of the Konink. Nederlandsche Stoomboot-Maatschappij, N.V. (Royal Netherlands Steamship Co.), Amsterdam, now being constructed at Krimpen aan der Ijssel by C. van der Giessen and Zonen.&lt;br /&gt;
&lt;br /&gt;
This engine, designated type TES456, has been designed specifically to meet the requirements of coasters and similar vessels and is a trunk piston unit built with six and eight cylinders with a bore of 450 mm., a piston stroke of 250 mm., and a maximum speed of 250 r.p.m. The normal output of&lt;br /&gt;
&lt;br /&gt;
the six-cylinder unit is 2,000 b.h.p. at 250 r.p.m., 1,800 b.h.p. at 225 r.p.m. and 1,600 b.h.p. at 200 r.p.m., but for this installation it is rated at 1,800 b.h.p. at 250 r.p.m. with an m.e.p. of 5&#039;1 kg./cm.2. Test bed trials have also been run of the turbocharged version of this unit, the TEBS456, designed for a normal service output of 2,400 b.h.p. at 250 r.p.m. and “excellent” results have been obtained. The pressure charged, eight-cylinder unit would give 3,200 b.h.p. at 250 r.p.m. The engine and shafting to be installed in the new ship have been built to comply with the requirements of Lloyd’s Register and the Finnish Ice Class 1A, and the main characteristics are tabulated below: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Werkspoor &#039;&#039;TES456&#039;&#039; engine&lt;br /&gt;
!&lt;br /&gt;
!&lt;br /&gt;
|-&lt;br /&gt;
|No. of cylinders&lt;br /&gt;
|4&lt;br /&gt;
|-&lt;br /&gt;
|Bore, mm.&lt;br /&gt;
|450&lt;br /&gt;
|-&lt;br /&gt;
|Stroke, mm.&lt;br /&gt;
|700&lt;br /&gt;
|-&lt;br /&gt;
|Maximum speed, r.p.m.&lt;br /&gt;
|250&lt;br /&gt;
|-&lt;br /&gt;
|Mean effective pressure, kg/cm²&lt;br /&gt;
|5.1&lt;br /&gt;
|-&lt;br /&gt;
|Normal b.h.p.&lt;br /&gt;
|1,800&lt;br /&gt;
|-&lt;br /&gt;
|Corresponding r.p.m&lt;br /&gt;
|250&lt;br /&gt;
|-&lt;br /&gt;
|Guaranteed fuel consumption, gr./b.h.p.-hr&lt;br /&gt;
|158&lt;br /&gt;
|-&lt;br /&gt;
|Lubricating oil consumption, gr./b.h.p.-hr&lt;br /&gt;
|1.8&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Capacities of Pumps&lt;br /&gt;
!&lt;br /&gt;
!Manometric head,&lt;br /&gt;
metres&lt;br /&gt;
!Litres/hr&lt;br /&gt;
|-&lt;br /&gt;
|F.W. Circulating pump&lt;br /&gt;
|12&lt;br /&gt;
|50000&lt;br /&gt;
|-&lt;br /&gt;
|S.W. circulating pump&lt;br /&gt;
|15&lt;br /&gt;
|50000&lt;br /&gt;
|-&lt;br /&gt;
|Lube oil pump&lt;br /&gt;
|55&lt;br /&gt;
|55000&lt;br /&gt;
|-&lt;br /&gt;
|Standby camshaft lube oil pump&lt;br /&gt;
|25&lt;br /&gt;
|1200&lt;br /&gt;
|-&lt;br /&gt;
|Standby atomizer cooling oil pump&lt;br /&gt;
|20&lt;br /&gt;
|900&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Weights&lt;br /&gt;
!&lt;br /&gt;
!Kg.&lt;br /&gt;
|-&lt;br /&gt;
|Engine, complete with integral thrust block and standard flywheel&lt;br /&gt;
|58000&lt;br /&gt;
|-&lt;br /&gt;
|Two air reservoirs&lt;br /&gt;
|3300&lt;br /&gt;
|-&lt;br /&gt;
|Silencer/spark arrester&lt;br /&gt;
|1500&lt;br /&gt;
|-&lt;br /&gt;
|Tools&lt;br /&gt;
|450&lt;br /&gt;
|-&lt;br /&gt;
|Lloyd’s Register’s spares&lt;br /&gt;
|2500&lt;br /&gt;
|-&lt;br /&gt;
|Oil and water in en&lt;br /&gt;
|1800&lt;br /&gt;
|}&lt;br /&gt;
The bedplate is of welded steel construction, as are the frames, which are arranged so that the pistons can be withdrawn through the large side inspection doors. Of cast iron construction, the cylinder block in the upper part contains the cooling water space and the camshaft housing, the lower part being the scavenging air reservoir. Inspection windows, with wipers in the covers of the receiver space, give a view of the scavenging ports so that to some extent the pistons can be observed in operation. The cylinder heads are of perlitic cast iron, each with two exhaust valves in water cooled housings. There is one scavenging air pump to each cylinder; each pump is driven off the piston by two levers and coupling rods. The pistons are composed of four parts: the oil cooled, light metal crown; the cast steel, or nodular cast iron, piston pin bearing, which transfers the forces acting on the piston crown to the piston pin; a thin piston pin bearing bush, and the skirt. Although the weights of the pumps are given in the adjoining table, there is none driven off the engine, such units being indeoendent and electrically driven.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, October 1958; Vol. 39, p. 303.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== &#039;&#039;Development of German Marine Engine&#039;&#039; ==&lt;br /&gt;
In reviewing the development of the Deutz V.M. marine engine, the author points out that important advances have been made in simplifying the engine controls and governing gear. Commencing with Series 5, the mechanical control of the starting valves was superseded by a pneumatic starting and reversing system. It is not unusual, in the case of a trawler, for example, for more than 1,000 reversing operations to be carried out in the course of a single trip, yet there has not been the slightest confirmation of the fears expressed in some quarters that cylinder heads or pistons might be adversely affected. In Series 5 engines the induction and exhaust passages have also been considerably enlarged compared with earlier versions, and to make this possible they are no longer located on one side of the cylinder head only, but on both sides. This layout has proved particularly suitable in conjunction with the Buchi exhaust-driven turbo-charger which has been fitted to a steadily increasing number of engines ever since 1927. The redesigning of the air and gas passages in the cylinder head has also proved beneficial in view of the fact that after only a few modifications the V.M. engine will run on a wide range of gases, such as producer gas (frequently used by vessels on inland waterways), and, in the stationary role, town gas, sewage gas and natural gas. A recent design feature of the Deutz V.M. engines is the flywheel brake which is applied whenever the engine is stopped—either from the engine control position or from some other point at any required distance. The flywheel brake is air-operated and cuts the duration of a reversing operation to a fraction of the time previously needed, e.g., from 40 sec. to 10 sec. The present Deutz production programme incorporates V.M. engines in the power range from 250 to 1,800 h.p. with 6 and 8 cylinders without and with exhaust turbo-charging. The speed range of the smaller units is 350 to 500 r.p.m.; the big units have 250 r.p.m.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;K. Schmidt, European Shipbuilding, Vol, 3, No. 2, 1954; pp. 38-41.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cold Starting of Small Engine ==&lt;br /&gt;
The British North Greenland Expedition is using in its headquarters establishment at Queen Louise Land, a Petter single-cylinder water-cooled oil engine and generator. That set has a strenuous life, particularly during the two mid-winter months when darkness persists all the way round the clock. During the winter the set is running for some twenty hours per day, but in summer for perhaps four hours daily. A 50-gallon water tank holds the coolant, and a paraffin stove has to be used to keep the water from freezing during non-running times. The normal routine is to drain the engine system after stopping and to thaw out the pipes with a blow-lamp in the morning. With an outside temperature of minus 40 deg. F., the temperature in the engine room has proved to be minus 5 deg. F. at waist height and minus 12 deg. F. at floor level during periods of engine shut down. After running, the temperature in the room rises to between 40 deg. F. and 45 deg. F. No trouble has been experienced, during a year’s service, with starting by hand; neither the flame starting aid provided nor the battery starters have had to be used. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Oil Engine and Gas Turbine, July 1954; Vol. 22, p. 81.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== &#039;&#039;River Tankers with Voith Schneider Propulsion&#039;&#039; ==&lt;br /&gt;
&#039;&#039;&#039;Shell-Mex&#039;&#039;&#039; and &#039;&#039;&#039;B.P.&#039;&#039;&#039;, Ltd., is in process of augmenting its fleet of estuarial and river craft for service in the Bristol Channel and Severn, and in the Medway, Thames, Humber and Trent. Ten vessels for this type of service have been or will be ordered from British shipyards for completion in 1955-56. When commissioned they will be employed in distributing petroleum products from the six United Kingdom refineries of Shell and Anglo-Iranian, and be dovetailed into the main distribution system of Shell-Mex and B.P., Ltd. The vessels will be Diesel-engined and built to &#039;&#039;&#039;Lloyd’s Register&#039;&#039;&#039; requirements. They will be fitted with modem radar equipment where desirable, and vessels so fitted will have telescopic masts of special design. The cargo pumps and pipelines installed will ensure the effective segregation of the petroleum products to be carried.&lt;br /&gt;
&lt;br /&gt;
Nine of the new vessels will have the &#039;&#039;&#039;Voith Schneider&#039;&#039;&#039; propeller as the means of propulsion. With vertical blades and aerofoil section rotating round a vertical axis, the &#039;&#039;&#039;Voith Schneider&#039;&#039;&#039; propeller will make it possible for the vessels to dispense with rudder, sternframe and ordinary steering mechanisms. The ships will have greater manoeuvrability than with the ordinary screw propeller, a factor of great importance in the trade in which they will be employed. Crew accommodation and facilities will be to the customary high standard of the company’s fleet. A new Shell-Mex and B.P. 530-tons coaster, now building at Clelands (Successors), Ltd., Wallsend-on-Tyne, will soon be launched. This vessel will be 160ft. long, with 29ft. beam, and a draught of lift. 3in. This new coaster, with the other ten vessels under construction, will bring the Shell-Mex and B.P. fleet of coastal, estuarial, bunkering and river craft to a total of forty-seven.&lt;br /&gt;
&lt;br /&gt;
— &#039;&#039;The Shipping World, 18th August 1954; Vol. 131, p. 190.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cas Turbine for Liberty Ship ==&lt;br /&gt;
In the United States eleven companies have submitted to the Maritime Administration seventeen proposals for the development and furnishing of a complete gas-turbine propulsion-power plant for experimental installation in a Liberty ship of the National Defence Reserve Fleet. The proposals are in response to invitations issued by the Maritime Administration as a first step toward development of a “power package” of advanced design. This will be employed and tested first in one of the Liberty ships of the reserve fleet and after evaluation will be made available for further conversions and modernization of existing vessels and for new ship construction. &lt;br /&gt;
&lt;br /&gt;
More than forty firms evidenced interest in this engine-improvement project. Included in the responses are two proposing use of devices of French manufacture and another proposing use of components of Swiss origin. All of the proposals are under intensive study by a specialized group and a thorough evaluation of all data submitted will be made. The plan to be utilized for the first Liberty ship conversion will be announced later.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—Marine Engineering, July 1954; Vol. 59, p. 102.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=872</id>
		<title>Engineering Abstracts 1959</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=872"/>
		<updated>2026-03-28T16:06:29Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at &#039;&#039;&#039;Gotaverken&#039;&#039;&#039; Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. &lt;br /&gt;
&lt;br /&gt;
The project prepared by &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. &lt;br /&gt;
&lt;br /&gt;
She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. &#039;&#039;&#039;Pielstick&#039;&#039;&#039; machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. &#039;&#039;&#039;SEMT-Pielstick&#039;&#039;&#039; engines are coupled to two shafts through an &#039;&#039;&#039;ASEA&#039;&#039;&#039; electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. &lt;br /&gt;
&lt;br /&gt;
To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). &lt;br /&gt;
&lt;br /&gt;
They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. &lt;br /&gt;
&lt;br /&gt;
They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. &lt;br /&gt;
&lt;br /&gt;
The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a &#039;&#039;&#039;British Polar Diesel&#039;&#039;&#039; engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. &lt;br /&gt;
&lt;br /&gt;
The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. &#039;&#039;&#039;Westinghouse&#039;&#039;&#039; type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. &lt;br /&gt;
&lt;br /&gt;
This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. &lt;br /&gt;
&lt;br /&gt;
The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. &lt;br /&gt;
&lt;br /&gt;
While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems.  &lt;br /&gt;
&lt;br /&gt;
Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber.  &lt;br /&gt;
&lt;br /&gt;
A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
The telescope valve engine is an improved four-stroke cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are also favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. &lt;br /&gt;
&lt;br /&gt;
Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. &lt;br /&gt;
&lt;br /&gt;
To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. &lt;br /&gt;
&lt;br /&gt;
The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. &lt;br /&gt;
&lt;br /&gt;
The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. &lt;br /&gt;
&lt;br /&gt;
For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. &lt;br /&gt;
&lt;br /&gt;
From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead &#039;&#039;&#039;Bolnes&#039;&#039;&#039; engine with a bore of 190 mm. This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. &lt;br /&gt;
&lt;br /&gt;
As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. &lt;br /&gt;
&lt;br /&gt;
The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The &#039;&#039;&#039;Stork&#039;&#039;&#039; marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. &lt;br /&gt;
&lt;br /&gt;
The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. &lt;br /&gt;
&lt;br /&gt;
The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. &lt;br /&gt;
&lt;br /&gt;
The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. &lt;br /&gt;
&lt;br /&gt;
The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. &lt;br /&gt;
&lt;br /&gt;
As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. &lt;br /&gt;
&lt;br /&gt;
The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder &#039;&#039;&#039;Doxford&#039;&#039;&#039; type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd.  &lt;br /&gt;
&lt;br /&gt;
The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; main engines. The installation, which has been built by &#039;&#039;&#039;Stothert and Pitt&#039;&#039;&#039;, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by &#039;&#039;&#039;Renold’s&#039;&#039;&#039; chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency.  &lt;br /&gt;
&lt;br /&gt;
There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr.  &lt;br /&gt;
&lt;br /&gt;
The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure.  &lt;br /&gt;
&lt;br /&gt;
Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “&#039;&#039;&#039;Bolnes&#039;&#039;&#039;” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the &#039;&#039;&#039;Graviner Manufacturing&#039;&#039;&#039; Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. &#039;&#039;&#039;Ruston and Hornsby&#039;&#039;&#039;, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of 10in., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the boat which drives a screw propeller so mounted on a support that the axis of the propeller is movable relative to the fore and aft axis of the boat for steering, the support itself being pivotable about a horizontal axis to lift the screw propeller clear of the water. In Fig. 1 the engine shaft extends in a fore and aft direction into the lower part of the chain case (36) to carry a chain sprocket (44). The shaft (29) which extends through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member lies within the chain case in the same plane as the sprocket (44) being adjacent with the upper end of the chain case. A sprocket chain (46) runs over the two sprockets. Two arms (47), pivotally mounted in the chain case and extending downwardly from their pivotal mountings, carry at their free ends sprockets (48) which engage the chain (46) inside its loop between the sprockets (44 and 45), the arms (47) being acted on by springs (49). The latter tend to urge the arms upwardly and outwardly. The upward and outward movement of the arms (47) is limited by stops (50) so as to ensure that they move through equal distances. It will be apparent that the propeller (26) can be lifted out of the water by rocking the L-shaped member (15, 16) rearwardly and upwardly about the trunnions (17) and such rocking movement will cause the sprocket (45) to swing downwardly and rearwardly. The upper part of the chain loop will tend to move downwardly with the sprocket (45) introducing slack in the chain (46) which will be taken up by upward movement of the idler sprockets (48). Ultimately, when the upper part of the chain (46) extends in a substantially straight line between the sprockets (48), as indidated in dotted lines in Fig. 2, the sprocket (45) will move away from the chain and the driving connexion between the engine and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Development of Borsig-Fiat Engine ==&lt;br /&gt;
[[File:1959 Borsig Fiat Fig 2.png|alt=Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C. |left|thumb|380x380px|&#039;&#039;Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C.&#039;&#039;]]&lt;br /&gt;
The Buries Markes motor ship &#039;&#039;La Selva,&#039;&#039; is equipped with a &#039;&#039;&#039;Borsig-Fiat&#039;&#039;&#039; engine with six cylinders, 680 mm. in diameter, having a piston stroke of 1,200 mm. and a normal output of 4,750 b.h.p. at 130 r.p.m. The fuel used is Bunker C, up to 3,500 sec. Redwood I at 100 deg. F. During the shop trials, an output of 3,550 b.h.p. was attained at 118 r.p.m., with a mean effective pressure of 5-2 kg./sq. cm., when the turbochargers were out of action and air was drawn in directly from the engine room to the piston scavenge pumps. &lt;br /&gt;
&lt;br /&gt;
This output corresponds to 75 per cent of the full load power according to the propeller curve, whilst the m.e.p. value is similar to that with the unsupercharged engine. The exhaust temperature before the turbines did not exceed the normal value of 320 deg. C. and the change over from non-turbocharged operation to turbocharging could be made in a very short time. &lt;br /&gt;
[[File:1959 Borsig Fiat Fig 3.png|alt=Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. |thumb|250x250px|Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. ]]&lt;br /&gt;
Thus, all that was needed to attain 75 per cent output without turbocharging was to lock the turbocharger rotors and remove two manhole covers. Further developments have been made in this model, the speed being raised to 140 r.p.m. and the mean pressure to 6-86 kg./sq. cm. Under these conditions the engine has an output of 5,580 b.h.p. The maximum output of 6,300 b.h.p. or 1,050 b.h.p. per cylinder at about 146 r.p.m. is attained with an m.e.p. of 7-4 kg./sq. cm., corresponding to a mean piston speed of 5-8 m./sec. This is the load which the engine is capable of delivering on the test bed and sea trials for a period of three hours. The rated cylinder output of 930 b.h.p. at 140 r.p.m. with an m.e.p. of 6-86 kg./sq. cm., is that for which the engine is designed on the basis of the prevailing rules of the classification societies. The recommended output for continuous service is 80 per cent to 95 per cent of the rated output, according to the actual service conditions, namely, length and severity of the voyages, the frequency and duration of harbour stops, the ambient conditions of the engine room, the quality of fuel and the state of maintenance of the engine. The Borsig-Fiat engine is exhaust turbocharged on the constant pressure series principle, the two exhaust turbochargers being of the &#039;&#039;&#039;BBC&#039;&#039;&#039;.VTR 500 type with voluted gas intakes. They are arranged ahead of the crosshead driven double acting piston scavenge pumps, the total volume of which is about 1-3 times that of the power cylinders. During the trials at the works, it was ascertained that the proportion of the compression work of the turbochargers increases with increasing engine load, while the proportion of the compression work of the engine driven scavenge pumps decreases. This characteristic is desirable from the standpoint of engine efficiency. At full load the turbochargers provide about 75 per cent of the total work required for the compression of the charging and scavenge air. Upon starting, when accelerating and in the low speed range, the piston scavenge pumps provide most of the air supply because the turbochargers do not then deliver their full capacity. In the lower speed ranges, as well as at higher speeds, the engine is readily responsive, with a smoke free exhaust. Detailed results of the tests of the 4,750-b.h.p. engine in the &#039;&#039;La Selva&#039;&#039; are shown in Fig. 2, whilst in Fig. 3 the results achieved with the engine after the further development are indicated. They show a total increase of 17-5 per cent, from 4,750 to 5,580 b.h.p., with a simultaneous rise of 130 r.p.m. to 140 r.p.m., or 7-8 per cent and a boost in b.m.e.p. from 6-3 kg. per sq. cm. to &#039;&#039;6-86&#039;&#039; kg. per sq. cm., or 9 per cent. The exhaust temperatures of the stepped-up 5,580-b.h.p. engine are 10 per cent higher whilst the charging air temperature after the blowers and before the scavenge ports, as well as the air pressure before the latter, have fallen slightly in spite of the increased boost. The ignition pressure of 65 kg. per sq. cm. when running on Diesel oil (60 kg. per sq. cm. when burning heavy fuel) remains the same. These improvements were rendered possible through higher efficiencies of the turbochargers, and improved adaptation of these blowers to the engine’s operating conditions. This also explains, for the most part, the reduction in specific fuel consumption from 164 gr. per b.h.p. per hr. to 156 gr. per b.h.p. per hr. or 4-7 per cent.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, May 1959; Vol. 40, pp. 86-87.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 24,000-b.H.p. Diesel Plant for Supertanker ==&lt;br /&gt;
[[File:1959 MAN 24000 BHP Diesel plant.png|alt=(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.|thumb|&#039;&#039;(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&#039;&#039;]]&lt;br /&gt;
In conjunction with a shipbuilding concern and a shipping company, the &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. have put forward plans for the propulsion machinery of 24,000 b.h.p. for a supertanker. The four engines are of standard &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. two-stroke type with 25 per cent turbocharging, the cylinders having a diameter of 570 mm. and a piston stroke of 800 mm. The speed is 225 r.p.m. The installation comprises two engines each of 7,300 b.h.p. driving a single shaft through hydraulic or electromagnetic couplings, and two engines of 6,000 b.h.p. in the wings and on a platform above the engine room floor, each driving an alternator supplying current to two 5,400-b.h.p. electric motors driving the same shaft through gearing. &lt;br /&gt;
&lt;br /&gt;
The total service output is 24,000 b.h.p. Current for the auxiliaries and for other ship requirements at sea is taken from the Diesel alternators so that no other Diesel generating plant is needed when under way. The four vertical cargo pumps are electrically driven, the electric motors being installed in the engine room. There are two Diesel generating sets for harbour and emergency duties and one gas turbine driven generator. The plant is installed in an engine room of the same size as that required for steam turbine and boiler plant. The fuel consumption is not as favourable as with the slower running, direct coupled units, the additional expenditure being about 10 gr./b.h.p.-hr., but it is considered that the saving compared with steam turbine plant is so great that this factor is not of importance.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 51.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Torque Transfer Coupling ==&lt;br /&gt;
[[File:1959 The Metalastik torque transfer coupling.png|alt=The Metalastik torque transfer coupling|left|thumb|&#039;&#039;(1959) The Metalastik torque transfer coupling&#039;&#039;]]&lt;br /&gt;
An interesting feature of the new range of Ruston high pressure turbocharged four-stroke engines is the new type flexible coupling with which they are fitted. These torque transfer couplings, developed by &#039;&#039;&#039;Metalastik&#039;&#039;&#039;, Ltd., are designed expressly to provide an effective and economical solution to the problem of resonant torsional vibration and the serious consequencies arising from it in marine and other installations. &lt;br /&gt;
&lt;br /&gt;
The Metalastik coupling is said to provide initially a very low stiffness with a much higher value for a predetermined torque. The ratio of initial and final stiffness can be varied as required, this being enabled by the fact that for low torques, rubber, loaded in torsional shear, is employed, while for higher torques separate rubber buffers, loaded in compression, provide the greater degree of stiffness required. There is a rather rapid change from low to high stiffness but the characteristics of the coupling can be modified to give a more gradual charge. In addition to its capacity to damp torsional vibrations the coupling is stated to be able to accommodate some malalignment. Basically the coupling consists of two sets of three rocker arms. These are connected at their extremities by means of special shackle pins. Each arm pivots centrally on a Metalastik bush. Rubber-bonded buffers are bolted to flats formed on three of the rocker arms. These come into contact with flats on the other set of rockers when a certain torque has been reached and the initial clearance has been taken up. One set of rockers is connected by three tapered pins to the flywheel and the other set by three pins to the gearbox flange, the inner sleeves of the centre pivot bushes being keyed to the pins.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 35.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Fuel Problems in Merchant Ships ==&lt;br /&gt;
The situation has developed where marine propulsion systems can only be competitive if they are capable of using the residual fuel oil which is marketed normally as Bunker C Grade. The nature of this oil is examined, the increases which have occurred in recent years in vanadium and sulphur content being noted. The influence of shipboard storage practice, with particular reference to sludge formation, is discussed; there are remarks on the reduced likelihood of salt water contamination. The main problems encountered in boilers are considered.&lt;br /&gt;
&lt;br /&gt;
Damage to brickwork is more a matter of spalling than of slag erosion. It is suggested that the significance of vanadium may have been overrated in the problem of bonded ash deposits in conventional marine boilers. The detrimental effect on boiler efficiency of the difficulties arising from the air heater corrosion and blocking is emphasized. Cylinder wear and sticking piston rings are among the difficulties encountered when burning residual fuel oil in large marine Diesel engines. The development of gas turbines for marine use has given rise to much work during the past ten years on the problems of ash fouling and corrosion. Some observations are made on the removal of sodium from the fuel by a water washing process incorporated into the fuel system.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. McClimont, Journal of the Institute of Fuel, May 1959; Vol. 32, pp. 225-231.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion of Ships at Sea ==&lt;br /&gt;
A general consideration of screw propulsion of ships at sea leads the author to a new approach to the analysis of seagoing performance, which is regarded as the result of interactions of the relevant characteristics of engine, propeller and hull. A discussion on the torque characteristics of reciprocating engines and turbines is followed by a consideration of propeller action as influenced by immersion and by its movements in a seaway. &lt;br /&gt;
&lt;br /&gt;
When the propeller torque and thrust characteristics are also accepted as variables, a simple analysis of known records for the &#039;&#039;Simon Bolivar,&#039;&#039; the &#039;&#039;Lubumbashi,&#039;&#039; the &#039;&#039;Tervate&#039;&#039; and the &#039;&#039;Nissei Maru&#039;&#039; shows that the data can be divided into one group with the propeller apparently unaffected by ship movements and waves, and another with the propeller so affected. The still water type of results allows some new conclusions to be drawn regarding wake, propeller characteristics, and the effect of small propeller immersions, which are also, in part, valid for model test conditions. &lt;br /&gt;
&lt;br /&gt;
The results affected by waves, etc., when combined with engine characteristics, show a typical difference between reciprocating engine drive and turbine drive at sea. A few general remarks on the results are concluded by a note on the possible use of the propulsion analysis in further investigation of ship resistance and movements in waves.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;J. Oervig, Norwegian Univ. Techn. Ship Model Tank Report No. 58, 1958. Journal, The British Shipbuilding Research Association, March 1959; Vol. 14, Abstract No. 15,070.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== New W erkspoor Engine for Coasters ==&lt;br /&gt;
The new design of Werkspoor uniflow scavenged, trunk piston engine, is to be installed in a new ship of the Konink. Nederlandsche Stoomboot-Maatschappij, N.V. (Royal Netherlands Steamship Co.), Amsterdam, now being constructed at Krimpen aan der Ijssel by C. van der Giessen and Zonen.&lt;br /&gt;
&lt;br /&gt;
This engine, designated type TES456, has been designed specifically to meet the requirements of coasters and similar vessels and is a trunk piston unit built with six and eight cylinders with a bore of 450 mm., a piston stroke of 250 mm., and a maximum speed of 250 r.p.m. The normal output of&lt;br /&gt;
&lt;br /&gt;
the six-cylinder unit is 2,000 b.h.p. at 250 r.p.m., 1,800 b.h.p. at 225 r.p.m. and 1,600 b.h.p. at 200 r.p.m., but for this installation it is rated at 1,800 b.h.p. at 250 r.p.m. with an m.e.p. of 5&#039;1 kg./cm.2. Test bed trials have also been run of the turbocharged version of this unit, the TEBS456, designed for a normal service output of 2,400 b.h.p. at 250 r.p.m. and “excellent” results have been obtained. The pressure charged, eight-cylinder unit would give 3,200 b.h.p. at 250 r.p.m. The engine and shafting to be installed in the new ship have been built to comply with the requirements of Lloyd’s Register and the Finnish Ice Class 1A, and the main characteristics are tabulated below: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Werkspoor &#039;&#039;TES456&#039;&#039; engine&lt;br /&gt;
!&lt;br /&gt;
!&lt;br /&gt;
|-&lt;br /&gt;
|No. of cylinders&lt;br /&gt;
|4&lt;br /&gt;
|-&lt;br /&gt;
|Bore, mm.&lt;br /&gt;
|450&lt;br /&gt;
|-&lt;br /&gt;
|Stroke, mm.&lt;br /&gt;
|700&lt;br /&gt;
|-&lt;br /&gt;
|Maximum speed, r.p.m.&lt;br /&gt;
|250&lt;br /&gt;
|-&lt;br /&gt;
|Mean effective pressure, kg/cm²&lt;br /&gt;
|5.1&lt;br /&gt;
|-&lt;br /&gt;
|Normal b.h.p.&lt;br /&gt;
|1,800&lt;br /&gt;
|-&lt;br /&gt;
|Corresponding r.p.m&lt;br /&gt;
|250&lt;br /&gt;
|-&lt;br /&gt;
|Guaranteed fuel consumption, gr./b.h.p.-hr&lt;br /&gt;
|158&lt;br /&gt;
|-&lt;br /&gt;
|Lubricating oil consumption, gr./b.h.p.-hr&lt;br /&gt;
|1.8&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Capacities of Pumps&lt;br /&gt;
!&lt;br /&gt;
!Manometric head,&lt;br /&gt;
metres&lt;br /&gt;
!Litres/hr&lt;br /&gt;
|-&lt;br /&gt;
|F.W. Circulating pump&lt;br /&gt;
|12&lt;br /&gt;
|50000&lt;br /&gt;
|-&lt;br /&gt;
|S.W. circulating pump&lt;br /&gt;
|15&lt;br /&gt;
|50000&lt;br /&gt;
|-&lt;br /&gt;
|Lube oil pump&lt;br /&gt;
|55&lt;br /&gt;
|55000&lt;br /&gt;
|-&lt;br /&gt;
|Standby camshaft lube oil pump&lt;br /&gt;
|25&lt;br /&gt;
|1200&lt;br /&gt;
|-&lt;br /&gt;
|Standby atomizer cooling oil pump&lt;br /&gt;
|20&lt;br /&gt;
|900&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Weights&lt;br /&gt;
!&lt;br /&gt;
!Kg.&lt;br /&gt;
|-&lt;br /&gt;
|Engine, complete with integral thrust block and standard flywheel&lt;br /&gt;
|58000&lt;br /&gt;
|-&lt;br /&gt;
|Two air reservoirs&lt;br /&gt;
|3300&lt;br /&gt;
|-&lt;br /&gt;
|Silencer/spark arrester&lt;br /&gt;
|1500&lt;br /&gt;
|-&lt;br /&gt;
|Tools&lt;br /&gt;
|450&lt;br /&gt;
|-&lt;br /&gt;
|Lloyd’s Register’s spares&lt;br /&gt;
|2500&lt;br /&gt;
|-&lt;br /&gt;
|Oil and water in en&lt;br /&gt;
|1800&lt;br /&gt;
|}&lt;br /&gt;
The bedplate is of welded steel construction, as are the frames, which are arranged so that the pistons can be withdrawn through the large side inspection doors. Of cast iron construction, the cylinder block in the upper part contains the cooling water space and the camshaft housing, the lower part being the scavenging air reservoir. Inspection windows, with wipers in the covers of the receiver space, give a view of the scavenging ports so that to some extent the pistons can be observed in operation. The cylinder heads are of perlitic cast iron, each with two exhaust valves in water cooled housings. There is one scavenging air pump to each cylinder; each pump is driven off the piston by two levers and coupling rods. The pistons are composed of four parts: the oil cooled, light metal crown; the cast steel, or nodular cast iron, piston pin bearing, which transfers the forces acting on the piston crown to the piston pin; a thin piston pin bearing bush, and the skirt. Although the weights of the pumps are given in the adjoining table, there is none driven off the engine, such units being indeoendent and electrically driven.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, October 1958; Vol. 39, p. 303.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== &#039;&#039;Development of German Marine Engine&#039;&#039; ==&lt;br /&gt;
In reviewing the development of the Deutz V.M. marine engine, the author points out that important advances have been made in simplifying the engine controls and governing gear. Commencing with Series 5, the mechanical control of the starting valves was superseded by a pneumatic starting and reversing system. It is not unusual, in the case of a trawler, for example, for more than 1,000 reversing operations to be carried out in the course of a single trip, yet there has not been the slightest confirmation of the fears expressed in some quarters that cylinder heads or pistons might be adversely affected. In Series 5 engines the induction and exhaust passages have also been considerably enlarged compared with earlier versions, and to make this possible they are no longer located on one side of the cylinder head only, but on both sides. This layout has proved particularly suitable in conjunction with the Buchi exhaust-driven turbo-charger which has been fitted to a steadily increasing number of engines ever since 1927. The redesigning of the air and gas passages in the cylinder head has also proved beneficial in view of the fact that after only a few modifications the V.M. engine will run on a wide range of gases, such as producer gas (frequently used by vessels on inland waterways), and, in the stationary role, town gas, sewage gas and natural gas. A recent design feature of the Deutz V.M. engines is the flywheel brake which is applied whenever the engine is stopped—either from the engine control position or from some other point at any required distance. The flywheel brake is air-operated and cuts the duration of a reversing operation to a fraction of the time previously needed, e.g., from 40 sec. to 10 sec. The present Deutz production programme incorporates V.M. engines in the power range from 250 to 1,800 h.p. with 6 and 8 cylinders without and with exhaust turbo-charging. The speed range of the smaller units is 350 to 500 r.p.m.; the big units have 250 r.p.m.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;K. Schmidt, European Shipbuilding, Vol, 3, No. 2, 1954; pp. 38-41.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cold Starting of Small Engine ==&lt;br /&gt;
The British North Greenland Expedition is using in its headquarters establishment at Queen Louise Land, a Petter single-cylinder water-cooled oil engine and generator. That set has a strenuous life, particularly during the two mid-winter months when darkness persists all the way round the clock. During the winter the set is running for some twenty hours per day, but in summer for perhaps four hours daily. A 50-gallon water tank holds the coolant, and a paraffin stove has to be used to keep the water from freezing during non-running times. The normal routine is to drain the engine system after stopping and to thaw out the pipes with a blow-lamp in the morning. With an outside temperature of minus 40 deg. F., the temperature in the engine room has proved to be minus 5 deg. F. at waist height and minus 12 deg. F. at floor level during periods of engine shut down. After running, the temperature in the room rises to between 40 deg. F. and 45 deg. F. No trouble has been experienced, during a year’s service, with starting by hand; neither the flame starting aid provided nor the battery starters have had to be used. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Oil Engine and Gas Turbine, July 1954; Vol. 22, p. 81.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== &#039;&#039;River Tankers with Voith Schneider Propulsion&#039;&#039; ==&lt;br /&gt;
&#039;&#039;&#039;Shell-Mex&#039;&#039;&#039; and &#039;&#039;&#039;B.P.&#039;&#039;&#039;, Ltd., is in process of augmenting its fleet of estuarial and river craft for service in the Bristol Channel and Severn, and in the Medway, Thames, Humber and Trent. Ten vessels for this type of service have been or will be ordered from British shipyards for completion in 1955-56. When commissioned they will be employed in distributing petroleum products from the six United Kingdom refineries of Shell and Anglo-Iranian, and be dovetailed into the main distribution system of Shell-Mex and B.P., Ltd. The vessels will be Diesel-engined and built to &#039;&#039;&#039;Lloyd’s Register&#039;&#039;&#039; requirements. They will be fitted with modem radar equipment where desirable, and vessels so fitted will have telescopic masts of special design. The cargo pumps and pipelines installed will ensure the effective segregation of the petroleum products to be carried.&lt;br /&gt;
&lt;br /&gt;
Nine of the new vessels will have the &#039;&#039;&#039;Voith Schneider&#039;&#039;&#039; propeller as the means of propulsion. With vertical blades and aerofoil section rotating round a vertical axis, the &#039;&#039;&#039;Voith Schneider&#039;&#039;&#039; propeller will make it possible for the vessels to dispense with rudder, sternframe and ordinary steering mechanisms. The ships will have greater manoeuvrability than with the ordinary screw propeller, a factor of great importance in the trade in which they will be employed. Crew accommodation and facilities will be to the customary high standard of the company’s fleet. A new Shell-Mex and B.P. 530-tons coaster, now building at Clelands (Successors), Ltd., Wallsend-on-Tyne, will soon be launched. This vessel will be 160ft. long, with 29ft. beam, and a draught of lift. 3in. This new coaster, with the other ten vessels under construction, will bring the Shell-Mex and B.P. fleet of coastal, estuarial, bunkering and river craft to a total of forty-seven.&lt;br /&gt;
&lt;br /&gt;
— &#039;&#039;The Shipping World, 18th August 1954; Vol. 131, p. 190.&#039;&#039;&lt;/div&gt;</summary>
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&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at &#039;&#039;&#039;Gotaverken&#039;&#039;&#039; Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. &lt;br /&gt;
&lt;br /&gt;
The project prepared by &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. &lt;br /&gt;
&lt;br /&gt;
She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. &#039;&#039;&#039;Pielstick&#039;&#039;&#039; machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. &#039;&#039;&#039;SEMT-Pielstick&#039;&#039;&#039; engines are coupled to two shafts through an &#039;&#039;&#039;ASEA&#039;&#039;&#039; electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. &lt;br /&gt;
&lt;br /&gt;
To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). &lt;br /&gt;
&lt;br /&gt;
They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. &lt;br /&gt;
&lt;br /&gt;
They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. &lt;br /&gt;
&lt;br /&gt;
The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a &#039;&#039;&#039;British Polar Diesel&#039;&#039;&#039; engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. &lt;br /&gt;
&lt;br /&gt;
The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. &#039;&#039;&#039;Westinghouse&#039;&#039;&#039; type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. &lt;br /&gt;
&lt;br /&gt;
This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. &lt;br /&gt;
&lt;br /&gt;
The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. &lt;br /&gt;
&lt;br /&gt;
While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems.  &lt;br /&gt;
&lt;br /&gt;
Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber.  &lt;br /&gt;
&lt;br /&gt;
A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
The telescope valve engine is an improved four-stroke cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are also favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. &lt;br /&gt;
&lt;br /&gt;
Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. &lt;br /&gt;
&lt;br /&gt;
To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. &lt;br /&gt;
&lt;br /&gt;
The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. &lt;br /&gt;
&lt;br /&gt;
The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. &lt;br /&gt;
&lt;br /&gt;
For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. &lt;br /&gt;
&lt;br /&gt;
From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead &#039;&#039;&#039;Bolnes&#039;&#039;&#039; engine with a bore of 190 mm. This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. &lt;br /&gt;
&lt;br /&gt;
As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. &lt;br /&gt;
&lt;br /&gt;
The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The &#039;&#039;&#039;Stork&#039;&#039;&#039; marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. &lt;br /&gt;
&lt;br /&gt;
The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. &lt;br /&gt;
&lt;br /&gt;
The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. &lt;br /&gt;
&lt;br /&gt;
The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. &lt;br /&gt;
&lt;br /&gt;
The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. &lt;br /&gt;
&lt;br /&gt;
As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. &lt;br /&gt;
&lt;br /&gt;
The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder &#039;&#039;&#039;Doxford&#039;&#039;&#039; type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd.  &lt;br /&gt;
&lt;br /&gt;
The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; main engines. The installation, which has been built by &#039;&#039;&#039;Stothert and Pitt&#039;&#039;&#039;, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by &#039;&#039;&#039;Renold’s&#039;&#039;&#039; chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency.  &lt;br /&gt;
&lt;br /&gt;
There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr.  &lt;br /&gt;
&lt;br /&gt;
The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure.  &lt;br /&gt;
&lt;br /&gt;
Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “&#039;&#039;&#039;Bolnes&#039;&#039;&#039;” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the &#039;&#039;&#039;Graviner Manufacturing&#039;&#039;&#039; Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. &#039;&#039;&#039;Ruston and Hornsby&#039;&#039;&#039;, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of 10in., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the boat which drives a screw propeller so mounted on a support that the axis of the propeller is movable relative to the fore and aft axis of the boat for steering, the support itself being pivotable about a horizontal axis to lift the screw propeller clear of the water. In Fig. 1 the engine shaft extends in a fore and aft direction into the lower part of the chain case (36) to carry a chain sprocket (44). The shaft (29) which extends through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member lies within the chain case in the same plane as the sprocket (44) being adjacent with the upper end of the chain case. A sprocket chain (46) runs over the two sprockets. Two arms (47), pivotally mounted in the chain case and extending downwardly from their pivotal mountings, carry at their free ends sprockets (48) which engage the chain (46) inside its loop between the sprockets (44 and 45), the arms (47) being acted on by springs (49). The latter tend to urge the arms upwardly and outwardly. The upward and outward movement of the arms (47) is limited by stops (50) so as to ensure that they move through equal distances. It will be apparent that the propeller (26) can be lifted out of the water by rocking the L-shaped member (15, 16) rearwardly and upwardly about the trunnions (17) and such rocking movement will cause the sprocket (45) to swing downwardly and rearwardly. The upper part of the chain loop will tend to move downwardly with the sprocket (45) introducing slack in the chain (46) which will be taken up by upward movement of the idler sprockets (48). Ultimately, when the upper part of the chain (46) extends in a substantially straight line between the sprockets (48), as indidated in dotted lines in Fig. 2, the sprocket (45) will move away from the chain and the driving connexion between the engine and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Development of Borsig-Fiat Engine ==&lt;br /&gt;
[[File:1959 Borsig Fiat Fig 2.png|alt=Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C. |left|thumb|380x380px|&#039;&#039;Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C.&#039;&#039;]]&lt;br /&gt;
The Buries Markes motor ship &#039;&#039;La Selva,&#039;&#039; is equipped with a &#039;&#039;&#039;Borsig-Fiat&#039;&#039;&#039; engine with six cylinders, 680 mm. in diameter, having a piston stroke of 1,200 mm. and a normal output of 4,750 b.h.p. at 130 r.p.m. The fuel used is Bunker C, up to 3,500 sec. Redwood I at 100 deg. F. During the shop trials, an output of 3,550 b.h.p. was attained at 118 r.p.m., with a mean effective pressure of 5-2 kg./sq. cm., when the turbochargers were out of action and air was drawn in directly from the engine room to the piston scavenge pumps. &lt;br /&gt;
&lt;br /&gt;
This output corresponds to 75 per cent of the full load power according to the propeller curve, whilst the m.e.p. value is similar to that with the unsupercharged engine. The exhaust temperature before the turbines did not exceed the normal value of 320 deg. C. and the change over from non-turbocharged operation to turbocharging could be made in a very short time. &lt;br /&gt;
[[File:1959 Borsig Fiat Fig 3.png|alt=Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. |thumb|250x250px|Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. ]]&lt;br /&gt;
Thus, all that was needed to attain 75 per cent output without turbocharging was to lock the turbocharger rotors and remove two manhole covers. Further developments have been made in this model, the speed being raised to 140 r.p.m. and the mean pressure to 6-86 kg./sq. cm. Under these conditions the engine has an output of 5,580 b.h.p. The maximum output of 6,300 b.h.p. or 1,050 b.h.p. per cylinder at about 146 r.p.m. is attained with an m.e.p. of 7-4 kg./sq. cm., corresponding to a mean piston speed of 5-8 m./sec. This is the load which the engine is capable of delivering on the test bed and sea trials for a period of three hours. The rated cylinder output of 930 b.h.p. at 140 r.p.m. with an m.e.p. of 6-86 kg./sq. cm., is that for which the engine is designed on the basis of the prevailing rules of the classification societies. The recommended output for continuous service is 80 per cent to 95 per cent of the rated output, according to the actual service conditions, namely, length and severity of the voyages, the frequency and duration of harbour stops, the ambient conditions of the engine room, the quality of fuel and the state of maintenance of the engine. The Borsig-Fiat engine is exhaust turbocharged on the constant pressure series principle, the two exhaust turbochargers being of the &#039;&#039;&#039;BBC&#039;&#039;&#039;.VTR 500 type with voluted gas intakes. They are arranged ahead of the crosshead driven double acting piston scavenge pumps, the total volume of which is about 1-3 times that of the power cylinders. During the trials at the works, it was ascertained that the proportion of the compression work of the turbochargers increases with increasing engine load, while the proportion of the compression work of the engine driven scavenge pumps decreases. This characteristic is desirable from the standpoint of engine efficiency. At full load the turbochargers provide about 75 per cent of the total work required for the compression of the charging and scavenge air. Upon starting, when accelerating and in the low speed range, the piston scavenge pumps provide most of the air supply because the turbochargers do not then deliver their full capacity. In the lower speed ranges, as well as at higher speeds, the engine is readily responsive, with a smoke free exhaust. Detailed results of the tests of the 4,750-b.h.p. engine in the &#039;&#039;La Selva&#039;&#039; are shown in Fig. 2, whilst in Fig. 3 the results achieved with the engine after the further development are indicated. They show a total increase of 17-5 per cent, from 4,750 to 5,580 b.h.p., with a simultaneous rise of 130 r.p.m. to 140 r.p.m., or 7-8 per cent and a boost in b.m.e.p. from 6-3 kg. per sq. cm. to &#039;&#039;6-86&#039;&#039; kg. per sq. cm., or 9 per cent. The exhaust temperatures of the stepped-up 5,580-b.h.p. engine are 10 per cent higher whilst the charging air temperature after the blowers and before the scavenge ports, as well as the air pressure before the latter, have fallen slightly in spite of the increased boost. The ignition pressure of 65 kg. per sq. cm. when running on Diesel oil (60 kg. per sq. cm. when burning heavy fuel) remains the same. These improvements were rendered possible through higher efficiencies of the turbochargers, and improved adaptation of these blowers to the engine’s operating conditions. This also explains, for the most part, the reduction in specific fuel consumption from 164 gr. per b.h.p. per hr. to 156 gr. per b.h.p. per hr. or 4-7 per cent.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, May 1959; Vol. 40, pp. 86-87.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 24,000-b.H.p. Diesel Plant for Supertanker ==&lt;br /&gt;
[[File:1959 MAN 24000 BHP Diesel plant.png|alt=(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.|thumb|&#039;&#039;(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&#039;&#039;]]&lt;br /&gt;
In conjunction with a shipbuilding concern and a shipping company, the &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. have put forward plans for the propulsion machinery of 24,000 b.h.p. for a supertanker. The four engines are of standard &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. two-stroke type with 25 per cent turbocharging, the cylinders having a diameter of 570 mm. and a piston stroke of 800 mm. The speed is 225 r.p.m. The installation comprises two engines each of 7,300 b.h.p. driving a single shaft through hydraulic or electromagnetic couplings, and two engines of 6,000 b.h.p. in the wings and on a platform above the engine room floor, each driving an alternator supplying current to two 5,400-b.h.p. electric motors driving the same shaft through gearing. &lt;br /&gt;
&lt;br /&gt;
The total service output is 24,000 b.h.p. Current for the auxiliaries and for other ship requirements at sea is taken from the Diesel alternators so that no other Diesel generating plant is needed when under way. The four vertical cargo pumps are electrically driven, the electric motors being installed in the engine room. There are two Diesel generating sets for harbour and emergency duties and one gas turbine driven generator. The plant is installed in an engine room of the same size as that required for steam turbine and boiler plant. The fuel consumption is not as favourable as with the slower running, direct coupled units, the additional expenditure being about 10 gr./b.h.p.-hr., but it is considered that the saving compared with steam turbine plant is so great that this factor is not of importance.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 51.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Torque Transfer Coupling ==&lt;br /&gt;
[[File:1959 The Metalastik torque transfer coupling.png|alt=The Metalastik torque transfer coupling|left|thumb|&#039;&#039;(1959) The Metalastik torque transfer coupling&#039;&#039;]]&lt;br /&gt;
An interesting feature of the new range of Ruston high pressure turbocharged four-stroke engines is the new type flexible coupling with which they are fitted. These torque transfer couplings, developed by &#039;&#039;&#039;Metalastik&#039;&#039;&#039;, Ltd., are designed expressly to provide an effective and economical solution to the problem of resonant torsional vibration and the serious consequencies arising from it in marine and other installations. &lt;br /&gt;
&lt;br /&gt;
The Metalastik coupling is said to provide initially a very low stiffness with a much higher value for a predetermined torque. The ratio of initial and final stiffness can be varied as required, this being enabled by the fact that for low torques, rubber, loaded in torsional shear, is employed, while for higher torques separate rubber buffers, loaded in compression, provide the greater degree of stiffness required. There is a rather rapid change from low to high stiffness but the characteristics of the coupling can be modified to give a more gradual charge. In addition to its capacity to damp torsional vibrations the coupling is stated to be able to accommodate some malalignment. Basically the coupling consists of two sets of three rocker arms. These are connected at their extremities by means of special shackle pins. Each arm pivots centrally on a Metalastik bush. Rubber-bonded buffers are bolted to flats formed on three of the rocker arms. These come into contact with flats on the other set of rockers when a certain torque has been reached and the initial clearance has been taken up. One set of rockers is connected by three tapered pins to the flywheel and the other set by three pins to the gearbox flange, the inner sleeves of the centre pivot bushes being keyed to the pins.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 35.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Fuel Problems in Merchant Ships ==&lt;br /&gt;
The situation has developed where marine propulsion systems can only be competitive if they are capable of using the residual fuel oil which is marketed normally as Bunker C Grade. The nature of this oil is examined, the increases which have occurred in recent years in vanadium and sulphur content being noted. The influence of shipboard storage practice, with particular reference to sludge formation, is discussed; there are remarks on the reduced likelihood of salt water contamination. The main problems encountered in boilers are considered.&lt;br /&gt;
&lt;br /&gt;
Damage to brickwork is more a matter of spalling than of slag erosion. It is suggested that the significance of vanadium may have been overrated in the problem of bonded ash deposits in conventional marine boilers. The detrimental effect on boiler efficiency of the difficulties arising from the air heater corrosion and blocking is emphasized. Cylinder wear and sticking piston rings are among the difficulties encountered when burning residual fuel oil in large marine Diesel engines. The development of gas turbines for marine use has given rise to much work during the past ten years on the problems of ash fouling and corrosion. Some observations are made on the removal of sodium from the fuel by a water washing process incorporated into the fuel system.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. McClimont, Journal of the Institute of Fuel, May 1959; Vol. 32, pp. 225-231.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion of Ships at Sea ==&lt;br /&gt;
A general consideration of screw propulsion of ships at sea leads the author to a new approach to the analysis of seagoing performance, which is regarded as the result of interactions of the relevant characteristics of engine, propeller and hull. A discussion on the torque characteristics of reciprocating engines and turbines is followed by a consideration of propeller action as influenced by immersion and by its movements in a seaway. &lt;br /&gt;
&lt;br /&gt;
When the propeller torque and thrust characteristics are also accepted as variables, a simple analysis of known records for the &#039;&#039;Simon Bolivar,&#039;&#039; the &#039;&#039;Lubumbashi,&#039;&#039; the &#039;&#039;Tervate&#039;&#039; and the &#039;&#039;Nissei Maru&#039;&#039; shows that the data can be divided into one group with the propeller apparently unaffected by ship movements and waves, and another with the propeller so affected. The still water type of results allows some new conclusions to be drawn regarding wake, propeller characteristics, and the effect of small propeller immersions, which are also, in part, valid for model test conditions. &lt;br /&gt;
&lt;br /&gt;
The results affected by waves, etc., when combined with engine characteristics, show a typical difference between reciprocating engine drive and turbine drive at sea. A few general remarks on the results are concluded by a note on the possible use of the propulsion analysis in further investigation of ship resistance and movements in waves.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;J. Oervig, Norwegian Univ. Techn. Ship Model Tank Report No. 58, 1958. Journal, The British Shipbuilding Research Association, March 1959; Vol. 14, Abstract No. 15,070.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== New W erkspoor Engine for Coasters ==&lt;br /&gt;
The new design of Werkspoor uniflow scavenged, trunk piston engine, is to be installed in a new ship of the Konink. Nederlandsche Stoomboot-Maatschappij, N.V. (Royal Netherlands Steamship Co.), Amsterdam, now being constructed at Krimpen aan der Ijssel by C. van der Giessen and Zonen.&lt;br /&gt;
&lt;br /&gt;
This engine, designated type TES456, has been designed specifically to meet the requirements of coasters and similar vessels and is a trunk piston unit built with six and eight cylinders with a bore of 450 mm., a piston stroke of 250 mm., and a maximum speed of 250 r.p.m. The normal output of&lt;br /&gt;
&lt;br /&gt;
the six-cylinder unit is 2,000 b.h.p. at 250 r.p.m., 1,800 b.h.p. at 225 r.p.m. and 1,600 b.h.p. at 200 r.p.m., but for this installation it is rated at 1,800 b.h.p. at 250 r.p.m. with an m.e.p. of 5&#039;1 kg./cm.2. Test bed trials have also been run of the turbocharged version of this unit, the TEBS456, designed for a normal service output of 2,400 b.h.p. at 250 r.p.m. and “excellent” results have been obtained. The pressure charged, eight-cylinder unit would give 3,200 b.h.p. at 250 r.p.m. The engine and shafting to be installed in the new ship have been built to comply with the requirements of Lloyd’s Register and the Finnish Ice Class 1A, and the main characteristics are tabulated below: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Werkspoor &#039;&#039;TES456&#039;&#039; engine&lt;br /&gt;
!&lt;br /&gt;
!&lt;br /&gt;
|-&lt;br /&gt;
|No. of cylinders&lt;br /&gt;
|4&lt;br /&gt;
|-&lt;br /&gt;
|Bore, mm.&lt;br /&gt;
|450&lt;br /&gt;
|-&lt;br /&gt;
|Stroke, mm.&lt;br /&gt;
|700&lt;br /&gt;
|-&lt;br /&gt;
|Maximum speed, r.p.m.&lt;br /&gt;
|250&lt;br /&gt;
|-&lt;br /&gt;
|Mean effective pressure, kg/cm²&lt;br /&gt;
|5.1&lt;br /&gt;
|-&lt;br /&gt;
|Normal b.h.p.&lt;br /&gt;
|1,800&lt;br /&gt;
|-&lt;br /&gt;
|Corresponding r.p.m&lt;br /&gt;
|250&lt;br /&gt;
|-&lt;br /&gt;
|Guaranteed fuel consumption, gr./b.h.p.-hr&lt;br /&gt;
|158&lt;br /&gt;
|-&lt;br /&gt;
|Lubricating oil consumption, gr./b.h.p.-hr&lt;br /&gt;
|1.8&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Capacities of Pumps&lt;br /&gt;
!&lt;br /&gt;
!Manometric head,&lt;br /&gt;
metres&lt;br /&gt;
!Litres/hr&lt;br /&gt;
|-&lt;br /&gt;
|F.W. Circulating pump&lt;br /&gt;
|12&lt;br /&gt;
|50000&lt;br /&gt;
|-&lt;br /&gt;
|S.W. circulating pump&lt;br /&gt;
|15&lt;br /&gt;
|50000&lt;br /&gt;
|-&lt;br /&gt;
|Lube oil pump&lt;br /&gt;
|55&lt;br /&gt;
|55000&lt;br /&gt;
|-&lt;br /&gt;
|Standby camshaft lube oil pump&lt;br /&gt;
|25&lt;br /&gt;
|1200&lt;br /&gt;
|-&lt;br /&gt;
|Standby atomizer cooling oil pump&lt;br /&gt;
|20&lt;br /&gt;
|900&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+Weights&lt;br /&gt;
!&lt;br /&gt;
!Kg.&lt;br /&gt;
|-&lt;br /&gt;
|Engine, complete with integral thrust block and standard flywheel&lt;br /&gt;
|58000&lt;br /&gt;
|-&lt;br /&gt;
|Two air reservoirs&lt;br /&gt;
|3300&lt;br /&gt;
|-&lt;br /&gt;
|Silencer/spark arrester&lt;br /&gt;
|1500&lt;br /&gt;
|-&lt;br /&gt;
|Tools&lt;br /&gt;
|450&lt;br /&gt;
|-&lt;br /&gt;
|Lloyd’s Register’s spares&lt;br /&gt;
|2500&lt;br /&gt;
|-&lt;br /&gt;
|Oil and water in en&lt;br /&gt;
|1800&lt;br /&gt;
|}&lt;br /&gt;
The bedplate is of welded steel construction, as are the frames, which are arranged so that the pistons can be withdrawn through the large side inspection doors. Of cast iron construction, the cylinder block in the upper part contains the cooling water space and the camshaft housing, the lower part being the scavenging air reservoir. Inspection windows, with wipers in the covers of the receiver space, give a view of the scavenging ports so that to some extent the pistons can be observed in operation. The cylinder heads are of perlitic cast iron, each with two exhaust valves in water cooled housings. There is one scavenging air pump to each cylinder; each pump is driven off the piston by two levers and coupling rods. The pistons are composed of four parts: the oil cooled, light metal crown; the cast steel, or nodular cast iron, piston pin bearing, which transfers the forces acting on the piston crown to the piston pin; a thin piston pin bearing bush, and the skirt. Although the weights of the pumps are given in the adjoining table, there is none driven off the engine, such units being indeoendent and electrically driven.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, October 1958; Vol. 39, p. 303.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=869</id>
		<title>Engineering Abstracts 1959</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=869"/>
		<updated>2026-03-28T12:39:44Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at &#039;&#039;&#039;Gotaverken&#039;&#039;&#039; Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. &lt;br /&gt;
&lt;br /&gt;
The project prepared by &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The &#039;&#039;&#039;M.A.N.&#039;&#039;&#039; engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. &lt;br /&gt;
&lt;br /&gt;
She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. &#039;&#039;&#039;Pielstick&#039;&#039;&#039; machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. &#039;&#039;&#039;SEMT-Pielstick&#039;&#039;&#039; engines are coupled to two shafts through an &#039;&#039;&#039;ASEA&#039;&#039;&#039; electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. &lt;br /&gt;
&lt;br /&gt;
To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). &lt;br /&gt;
&lt;br /&gt;
They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. &lt;br /&gt;
&lt;br /&gt;
They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. &lt;br /&gt;
&lt;br /&gt;
The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a &#039;&#039;&#039;British Polar Diesel&#039;&#039;&#039; engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. &lt;br /&gt;
&lt;br /&gt;
The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. &#039;&#039;&#039;Westinghouse&#039;&#039;&#039; type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. &lt;br /&gt;
&lt;br /&gt;
This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. &lt;br /&gt;
&lt;br /&gt;
The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. &lt;br /&gt;
&lt;br /&gt;
While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems.  &lt;br /&gt;
&lt;br /&gt;
Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber.  &lt;br /&gt;
&lt;br /&gt;
A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
The telescope valve engine is an improved four-stroke cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are also favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. &lt;br /&gt;
&lt;br /&gt;
Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. &lt;br /&gt;
&lt;br /&gt;
To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. &lt;br /&gt;
&lt;br /&gt;
The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. &lt;br /&gt;
&lt;br /&gt;
The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. &lt;br /&gt;
&lt;br /&gt;
For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. &lt;br /&gt;
&lt;br /&gt;
From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead &#039;&#039;&#039;Bolnes&#039;&#039;&#039; engine with a bore of 190 mm. This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. &lt;br /&gt;
&lt;br /&gt;
As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. &lt;br /&gt;
&lt;br /&gt;
The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The &#039;&#039;&#039;Stork&#039;&#039;&#039; marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. &lt;br /&gt;
&lt;br /&gt;
The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. &lt;br /&gt;
&lt;br /&gt;
The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. &lt;br /&gt;
&lt;br /&gt;
The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. &lt;br /&gt;
&lt;br /&gt;
The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. &lt;br /&gt;
&lt;br /&gt;
As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. &lt;br /&gt;
&lt;br /&gt;
The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder &#039;&#039;&#039;Doxford&#039;&#039;&#039; type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd.  &lt;br /&gt;
&lt;br /&gt;
The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with &#039;&#039;&#039;Burmeister and Wain&#039;&#039;&#039; main engines. The installation, which has been built by &#039;&#039;&#039;Stothert and Pitt&#039;&#039;&#039;, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by &#039;&#039;&#039;Renold’s&#039;&#039;&#039; chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency.  &lt;br /&gt;
&lt;br /&gt;
There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr.  &lt;br /&gt;
&lt;br /&gt;
The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure.  &lt;br /&gt;
&lt;br /&gt;
Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “&#039;&#039;&#039;Bolnes&#039;&#039;&#039;” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the &#039;&#039;&#039;Graviner Manufacturing&#039;&#039;&#039; Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. &#039;&#039;&#039;Ruston and Hornsby&#039;&#039;&#039;, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of 10in., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the boat which drives a screw propeller so mounted on a support that the axis of the propeller is movable relative to the fore and aft axis of the boat for steering, the support itself being pivotable about a horizontal axis to lift the screw propeller clear of the water. In Fig. 1 the engine shaft extends in a fore and aft direction into the lower part of the chain case (36) to carry a chain sprocket (44). The shaft (29) which extends through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member lies within the chain case in the same plane as the sprocket (44) being adjacent with the upper end of the chain case. A sprocket chain (46) runs over the two sprockets. Two arms (47), pivotally mounted in the chain case and extending downwardly from their pivotal mountings, carry at their free ends sprockets (48) which engage the chain (46) inside its loop between the sprockets (44 and 45), the arms (47) being acted on by springs (49). The latter tend to urge the arms upwardly and outwardly. The upward and outward movement of the arms (47) is limited by stops (50) so as to ensure that they move through equal distances. It will be apparent that the propeller (26) can be lifted out of the water by rocking the L-shaped member (15, 16) rearwardly and upwardly about the trunnions (17) and such rocking movement will cause the sprocket (45) to swing downwardly and rearwardly. The upper part of the chain loop will tend to move downwardly with the sprocket (45) introducing slack in the chain (46) which will be taken up by upward movement of the idler sprockets (48). Ultimately, when the upper part of the chain (46) extends in a substantially straight line between the sprockets (48), as indidated in dotted lines in Fig. 2, the sprocket (45) will move away from the chain and the driving connexion between the engine and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Development of Borsig-Fiat Engine ==&lt;br /&gt;
[[File:1959 Borsig Fiat Fig 2.png|alt=Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C. |left|thumb|380x380px|&#039;&#039;Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C.&#039;&#039;]]&lt;br /&gt;
The Buries Markes motor ship &#039;&#039;La Selva,&#039;&#039; is equipped with a &#039;&#039;&#039;Borsig-Fiat&#039;&#039;&#039; engine with six cylinders, 680 mm. in diameter, having a piston stroke of 1,200 mm. and a normal output of 4,750 b.h.p. at 130 r.p.m. The fuel used is Bunker C, up to 3,500 sec. Redwood I at 100 deg. F. During the shop trials, an output of 3,550 b.h.p. was attained at 118 r.p.m., with a mean effective pressure of 5-2 kg./sq. cm., when the turbochargers were out of action and air was drawn in directly from the engine room to the piston scavenge pumps. &lt;br /&gt;
&lt;br /&gt;
This output corresponds to 75 per cent of the full load power according to the propeller curve, whilst the m.e.p. value is similar to that with the unsupercharged engine. The exhaust temperature before the turbines did not exceed the normal value of 320 deg. C. and the change over from non-turbocharged operation to turbocharging could be made in a very short time. &lt;br /&gt;
[[File:1959 Borsig Fiat Fig 3.png|alt=Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. |thumb|250x250px|Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. ]]&lt;br /&gt;
Thus, all that was needed to attain 75 per cent output without turbocharging was to lock the turbocharger rotors and remove two manhole covers. Further developments have been made in this model, the speed being raised to 140 r.p.m. and the mean pressure to 6-86 kg./sq. cm. Under these conditions the engine has an output of 5,580 b.h.p. The maximum output of 6,300 b.h.p. or 1,050 b.h.p. per cylinder at about 146 r.p.m. is attained with an m.e.p. of 7-4 kg./sq. cm., corresponding to a mean piston speed of 5-8 m./sec. This is the load which the engine is capable of delivering on the test bed and sea trials for a period of three hours. The rated cylinder output of 930 b.h.p. at 140 r.p.m. with an m.e.p. of 6-86 kg./sq. cm., is that for which the engine is designed on the basis of the prevailing rules of the classification societies. The recommended output for continuous service is 80 per cent to 95 per cent of the rated output, according to the actual service conditions, namely, length and severity of the voyages, the frequency and duration of harbour stops, the ambient conditions of the engine room, the quality of fuel and the state of maintenance of the engine. The Borsig-Fiat engine is exhaust turbocharged on the constant pressure series principle, the two exhaust turbochargers being of the &#039;&#039;&#039;BBC&#039;&#039;&#039;.VTR 500 type with voluted gas intakes. They are arranged ahead of the crosshead driven double acting piston scavenge pumps, the total volume of which is about 1-3 times that of the power cylinders. During the trials at the works, it was ascertained that the proportion of the compression work of the turbochargers increases with increasing engine load, while the proportion of the compression work of the engine driven scavenge pumps decreases. This characteristic is desirable from the standpoint of engine efficiency. At full load the turbochargers provide about 75 per cent of the total work required for the compression of the charging and scavenge air. Upon starting, when accelerating and in the low speed range, the piston scavenge pumps provide most of the air supply because the turbochargers do not then deliver their full capacity. In the lower speed ranges, as well as at higher speeds, the engine is readily responsive, with a smoke free exhaust. Detailed results of the tests of the 4,750-b.h.p. engine in the &#039;&#039;La Selva&#039;&#039; are shown in Fig. 2, whilst in Fig. 3 the results achieved with the engine after the further development are indicated. They show a total increase of 17-5 per cent, from 4,750 to 5,580 b.h.p., with a simultaneous rise of 130 r.p.m. to 140 r.p.m., or 7-8 per cent and a boost in b.m.e.p. from 6-3 kg. per sq. cm. to &#039;&#039;6-86&#039;&#039; kg. per sq. cm., or 9 per cent. The exhaust temperatures of the stepped-up 5,580-b.h.p. engine are 10 per cent higher whilst the charging air temperature after the blowers and before the scavenge ports, as well as the air pressure before the latter, have fallen slightly in spite of the increased boost. The ignition pressure of 65 kg. per sq. cm. when running on Diesel oil (60 kg. per sq. cm. when burning heavy fuel) remains the same. These improvements were rendered possible through higher efficiencies of the turbochargers, and improved adaptation of these blowers to the engine’s operating conditions. This also explains, for the most part, the reduction in specific fuel consumption from 164 gr. per b.h.p. per hr. to 156 gr. per b.h.p. per hr. or 4-7 per cent.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, May 1959; Vol. 40, pp. 86-87.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 24,000-b.H.p. Diesel Plant for Supertanker ==&lt;br /&gt;
[[File:1959 MAN 24000 BHP Diesel plant.png|alt=(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.|thumb|&#039;&#039;(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&#039;&#039;]]&lt;br /&gt;
In conjunction with a shipbuilding concern and a shipping company, the &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. have put forward plans for the propulsion machinery of 24,000 b.h.p. for a supertanker. The four engines are of standard &#039;&#039;&#039;M.A.N&#039;&#039;&#039;. two-stroke type with 25 per cent turbocharging, the cylinders having a diameter of 570 mm. and a piston stroke of 800 mm. The speed is 225 r.p.m. The installation comprises two engines each of 7,300 b.h.p. driving a single shaft through hydraulic or electromagnetic couplings, and two engines of 6,000 b.h.p. in the wings and on a platform above the engine room floor, each driving an alternator supplying current to two 5,400-b.h.p. electric motors driving the same shaft through gearing. &lt;br /&gt;
&lt;br /&gt;
The total service output is 24,000 b.h.p. Current for the auxiliaries and for other ship requirements at sea is taken from the Diesel alternators so that no other Diesel generating plant is needed when under way. The four vertical cargo pumps are electrically driven, the electric motors being installed in the engine room. There are two Diesel generating sets for harbour and emergency duties and one gas turbine driven generator. The plant is installed in an engine room of the same size as that required for steam turbine and boiler plant. The fuel consumption is not as favourable as with the slower running, direct coupled units, the additional expenditure being about 10 gr./b.h.p.-hr., but it is considered that the saving compared with steam turbine plant is so great that this factor is not of importance.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 51.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Torque Transfer Coupling ==&lt;br /&gt;
[[File:1959 The Metalastik torque transfer coupling.png|alt=The Metalastik torque transfer coupling|left|thumb|&#039;&#039;(1959) The Metalastik torque transfer coupling&#039;&#039;]]&lt;br /&gt;
An interesting feature of the new range of Ruston high pressure turbocharged four-stroke engines is the new type flexible coupling with which they are fitted. These torque transfer couplings, developed by &#039;&#039;&#039;Metalastik&#039;&#039;&#039;, Ltd., are designed expressly to provide an effective and economical solution to the problem of resonant torsional vibration and the serious consequencies arising from it in marine and other installations. &lt;br /&gt;
&lt;br /&gt;
The Metalastik coupling is said to provide initially a very low stiffness with a much higher value for a predetermined torque. The ratio of initial and final stiffness can be varied as required, this being enabled by the fact that for low torques, rubber, loaded in torsional shear, is employed, while for higher torques separate rubber buffers, loaded in compression, provide the greater degree of stiffness required. There is a rather rapid change from low to high stiffness but the characteristics of the coupling can be modified to give a more gradual charge. In addition to its capacity to damp torsional vibrations the coupling is stated to be able to accommodate some malalignment. Basically the coupling consists of two sets of three rocker arms. These are connected at their extremities by means of special shackle pins. Each arm pivots centrally on a Metalastik bush. Rubber-bonded buffers are bolted to flats formed on three of the rocker arms. These come into contact with flats on the other set of rockers when a certain torque has been reached and the initial clearance has been taken up. One set of rockers is connected by three tapered pins to the flywheel and the other set by three pins to the gearbox flange, the inner sleeves of the centre pivot bushes being keyed to the pins.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 35.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=File:1959_The_Metalastik_torque_transfer_coupling.png&amp;diff=868</id>
		<title>File:1959 The Metalastik torque transfer coupling.png</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=File:1959_The_Metalastik_torque_transfer_coupling.png&amp;diff=868"/>
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		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;The Metalastik torque transfer coupling&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=867</id>
		<title>Engineering Abstracts 1959</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: /* Propulsion System for Boats */&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder Doxford type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd. The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with Burmeister and Wain main engines. The installation, which has been built by Stothert and Pitt, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by Renold’s chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency. There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr. The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure. Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “Bolnes” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the Graviner Manufacturing Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. Ruston and Hornsby, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of lOjin., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the boat which drives a screw propeller so mounted on a support that the axis of the propeller is movable relative to the fore and aft axis of the boat for steering, the support itself being pivotable about a horizontal axis to lift the screw propeller clear of the water. In Fig. 1 the engine shaft extends in a fore and aft direction into the lower part of the chain case (36) to carry a chain sprocket (44). The shaft (29) which extends through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member lies within the chain case in the same plane as the sprocket (44) being adjacent with the upper end of the chain case. A sprocket chain (46) runs over the two sprockets. Two arms (47), pivotally mounted in the chain case and extending downwardly from their pivotal mountings, carry at their free ends sprockets (48) which engage the chain (46) inside its loop between the sprockets (44 and 45), the arms (47) being acted on by springs (49). The latter tend to urge the arms upwardly and outwardly. The upward and outward movement of the arms (47) is limited by stops (50) so as to ensure that they move through equal distances. It will be apparent that the propeller (26) can be lifted out of the water by rocking the L-shaped member (15, 16) rearwardly and upwardly about the trunnions (17) and such rocking movement will cause the sprocket (45) to swing downwardly and rearwardly. The upper part of the chain loop will tend to move downwardly with the sprocket (45) introducing slack in the chain (46) which will be taken up by upward movement of the idler sprockets (48). Ultimately, when the upper part of the chain (46) extends in a substantially straight line between the sprockets (48), as indidated in dotted lines in Fig. 2, the sprocket (45) will move away from the chain and the driving connexion between the engine and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Development of Borsig-Fiat Engine ==&lt;br /&gt;
[[File:1959 Borsig Fiat Fig 2.png|alt=Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C. |left|thumb|380x380px|&#039;&#039;Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C.&#039;&#039;]]&lt;br /&gt;
The Buries Markes motor ship &#039;&#039;La Selva,&#039;&#039; is equipped with a Borsig-Fiat engine with six cylinders, 680 mm. in diameter, having a piston stroke of 1,200 mm. and a normal output of 4,750 b.h.p. at 130 r.p.m. The fuel used is Bunker C, up to 3,500 sec. Redwood I at 100 deg. F. During the shop trials, an output of 3,550 b.h.p. was attained at 118 r.p.m., with a mean effective pressure of 5-2 kg./sq. cm., when the turbochargers were out of action and air was drawn in directly from the engine room to the piston scavenge pumps. &lt;br /&gt;
&lt;br /&gt;
This output corresponds to 75 per cent of the full load power according to the propeller curve, whilst the m.e.p. value is similar to that with the unsupercharged engine. The exhaust temperature before the turbines did not exceed the normal value of 320 deg. C. and the change over from non-turbocharged operation to turbocharging could be made in a very short time. &lt;br /&gt;
[[File:1959 Borsig Fiat Fig 3.png|alt=Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. |thumb|250x250px|Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. ]]&lt;br /&gt;
Thus, all that was needed to attain 75 per cent output without turbocharging was to lock the turbocharger rotors and remove two manhole covers. Further developments have been made in this model, the speed being raised to 140 r.p.m. and the mean pressure to 6-86 kg./sq. cm. Under these conditions the engine has an output of 5,580 b.h.p. The maximum output of 6,300 b.h.p. or 1,050 b.h.p. per cylinder at about 146 r.p.m. is attained with an m.e.p. of 7-4 kg./sq. cm., corresponding to a mean piston speed of 5-8 m./sec. This is the load which the engine is capable of delivering on the test bed and sea trials for a period of three hours. The rated cylinder output of 930 b.h.p. at 140 r.p.m. with an m.e.p. of 6-86 kg./sq. cm., is that for which the engine is designed on the basis of the prevailing rules of the classification societies. The recommended output for continuous service is 80 per cent to 95 per cent of the rated output, according to the actual service conditions, namely, length and severity of the voyages, the frequency and duration of harbour stops, the ambient conditions of the engine room, the quality of fuel and the state of maintenance of the engine. The Borsig-Fiat engine is exhaust turbocharged on the constant pressure series principle, the two exhaust turbochargers being of the BBC.VTR 500 type with voluted gas intakes. They are arranged ahead of the crosshead driven double acting piston scavenge pumps, the total volume of which is about 1-3 times that of the power cylinders. During the trials at the works, it was ascertained that the proportion of the compression work of the turbochargers increases with increasing engine load, while the proportion of the compression work of the engine driven scavenge pumps decreases. This characteristic is desirable from the standpoint of engine efficiency. At full load the turbochargers provide about 75 per cent of the total work required for the compression of the charging and scavenge air. Upon starting, when accelerating and in the low speed range, the piston scavenge pumps provide most of the air supply because the turbochargers do not then deliver their full capacity. In the lower speed ranges, as well as at higher speeds, the engine is readily responsive, with a smoke free exhaust. Detailed results of the tests of the 4,750-b.h.p. engine in the &#039;&#039;La Selva&#039;&#039; are shown in Fig. 2, whilst in Fig. 3 the results achieved with the engine after the further development are indicated. They show a total increase of 17-5 per cent, from 4,750 to 5,580 b.h.p., with a simultaneous rise of 130 r.p.m. to 140 r.p.m., or 7-8 per cent and a boost in b.m.e.p. from 6-3 kg. per sq. cm. to &#039;&#039;6-86&#039;&#039; kg. per sq. cm., or 9 per cent. The exhaust temperatures of the stepped-up 5,580-b.h.p. engine are 10 per cent higher whilst the charging air temperature after the blowers and before the scavenge ports, as well as the air pressure before the latter, have fallen slightly in spite of the increased boost. The ignition pressure of 65 kg. per sq. cm. when running on Diesel oil (60 kg. per sq. cm. when burning heavy fuel) remains the same. These improvements were rendered possible through higher efficiencies of the turbochargers, and improved adaptation of these blowers to the engine’s operating conditions. This also explains, for the most part, the reduction in specific fuel consumption from 164 gr. per b.h.p. per hr. to 156 gr. per b.h.p. per hr. or 4-7 per cent.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, May 1959; Vol. 40, pp. 86-87.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 24,000-b.H.p. Diesel Plant for Supertanker ==&lt;br /&gt;
[[File:1959 MAN 24000 BHP Diesel plant.png|alt=(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.|thumb|&#039;&#039;(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&#039;&#039;]]&lt;br /&gt;
In conjunction with a shipbuilding concern and a shipping company, the M.A.N. have put forward plans for the propulsion machinery of 24,000 b.h.p. for a supertanker. The four engines are of standard M.A.N. two-stroke type with 25 per cent turbocharging, the cylinders having a diameter of 570 mm. and a piston stroke of 800 mm. The speed is 225 r.p.m. The installation comprises two engines each of 7,300 b.h.p. driving a single shaft through hydraulic or electromagnetic couplings, and two engines of 6,000 b.h.p. in the wings and on a platform above the engine room floor, each driving an alternator supplying current to two 5,400-b.h.p. electric motors driving the same shaft through gearing. &lt;br /&gt;
&lt;br /&gt;
The total service output is 24,000 b.h.p. Current for the auxiliaries and for other ship requirements at sea is taken from the Diesel alternators so that no other Diesel generating plant is needed when under way. The four vertical cargo pumps are electrically driven, the electric motors being installed in the engine room. There are two Diesel generating sets for harbour and emergency duties and one gas turbine driven generator. The plant is installed in an engine room of the same size as that required for steam turbine and boiler plant. The fuel consumption is not as favourable as with the slower running, direct coupled units, the additional expenditure being about 10 gr./b.h.p.-hr., but it is considered that the saving compared with steam turbine plant is so great that this factor is not of importance.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 51.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1959</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: /* Engineering Abstracts from 1959 */&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder Doxford type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd. The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with Burmeister and Wain main engines. The installation, which has been built by Stothert and Pitt, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by Renold’s chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency. There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr. The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure. Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “Bolnes” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the Graviner Manufacturing Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. Ruston and Hornsby, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of lOjin., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the&lt;br /&gt;
&lt;br /&gt;
boat which drives a screw propeller so mounted on a support&lt;br /&gt;
&lt;br /&gt;
that the axis of the propeller is movable relative to the fore&lt;br /&gt;
&lt;br /&gt;
and aft axis of the boat for steering, the support itself being&lt;br /&gt;
&lt;br /&gt;
pivotable about a horizontal axis to lift the screw propeller&lt;br /&gt;
&lt;br /&gt;
clear of the water. In Fig. 1 the engine shaft extends in a&lt;br /&gt;
&lt;br /&gt;
fore and aft direction into the lower part of the chain case (36)&lt;br /&gt;
&lt;br /&gt;
to carry a chain sprocket (44). The shaft (29) which extends&lt;br /&gt;
&lt;br /&gt;
through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member&lt;br /&gt;
&lt;br /&gt;
lies within the chain case in the same plane as the sprocket&lt;br /&gt;
&lt;br /&gt;
(44) being adjacent with the upper end of the chain case. A&lt;br /&gt;
&lt;br /&gt;
sprocket chain (46) runs over the two sprockets. Two arms&lt;br /&gt;
&lt;br /&gt;
(47), pivotally mounted in the chain case and extending downwardly&lt;br /&gt;
&lt;br /&gt;
from their pivotal mountings, carry at their free ends&lt;br /&gt;
&lt;br /&gt;
sprockets (48) which engage the chain (46) inside its loop&lt;br /&gt;
&lt;br /&gt;
between the sprockets (44 and 45), the arms (47) being acted&lt;br /&gt;
&lt;br /&gt;
on by springs (49). The latter tend to urge the arms upwardly&lt;br /&gt;
&lt;br /&gt;
and outwardly. The upward and outward movement of the&lt;br /&gt;
&lt;br /&gt;
arms (47) is limited by stops (50) so as to ensure that they&lt;br /&gt;
&lt;br /&gt;
move through equal distances. It will be apparent that the&lt;br /&gt;
&lt;br /&gt;
propeller (26) can be lifted out of the water by rocking the&lt;br /&gt;
&lt;br /&gt;
L-shaped member (15, 16) rearwardly and upwardly about&lt;br /&gt;
&lt;br /&gt;
the trunnions (17) and such rocking movement will cause the&lt;br /&gt;
&lt;br /&gt;
sprocket (45) to swing downwardly and rearwardly. The upper&lt;br /&gt;
&lt;br /&gt;
part of the chain loop will tend to move downwardly with the&lt;br /&gt;
&lt;br /&gt;
sprocket (45) introducing slack in the chain (46) which will&lt;br /&gt;
&lt;br /&gt;
be taken up by upward movement of the idler sprockets (48).&lt;br /&gt;
&lt;br /&gt;
Ultimately, when the upper part of the chain (46) extends in&lt;br /&gt;
&lt;br /&gt;
a substantially straight line between the sprockets (48), as indidated&lt;br /&gt;
&lt;br /&gt;
in dotted lines in Fig. 2, the sprocket (45) will move away&lt;br /&gt;
&lt;br /&gt;
from the chain and the driving connexion between the engine&lt;br /&gt;
&lt;br /&gt;
and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Development of Borsig-Fiat Engine ==&lt;br /&gt;
[[File:1959 Borsig Fiat Fig 2.png|alt=Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C. |left|thumb|380x380px|&#039;&#039;Fig 2 —Test results of 4,750-b.h.p. six-cylinder turbocharged Borsig-Fiat engine. The fuel used was heavy oil with a viscosity of 2,470 secs. Redwood No. I at 100 deg. F. Sp. G. 0-954 at 15 deg. C.&#039;&#039;]]&lt;br /&gt;
The Buries Markes motor ship &#039;&#039;La Selva,&#039;&#039; is equipped with a Borsig-Fiat engine with six cylinders, 680 mm. in diameter, having a piston stroke of 1,200 mm. and a normal output of 4,750 b.h.p. at 130 r.p.m. The fuel used is Bunker C, up to 3,500 sec. Redwood I at 100 deg. F. During the shop trials, an output of 3,550 b.h.p. was attained at 118 r.p.m., with a mean effective pressure of 5-2 kg./sq. cm., when the turbochargers were out of action and air was drawn in directly from the engine room to the piston scavenge pumps. &lt;br /&gt;
&lt;br /&gt;
This output corresponds to 75 per cent of the full load power according to the propeller curve, whilst the m.e.p. value is similar to that with the unsupercharged engine. The exhaust temperature before the turbines did not exceed the normal value of 320 deg. C. and the change over from non-turbocharged operation to turbocharging could be made in a very short time. &lt;br /&gt;
[[File:1959 Borsig Fiat Fig 3.png|alt=Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. |thumb|250x250px|Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm. ]]&lt;br /&gt;
Thus, all that was needed to attain 75 per cent output without turbocharging was to lock the turbocharger rotors and remove two manhole covers. Further developments have been made in this model, the speed being raised to 140 r.p.m. and the mean pressure to 6-86 kg./sq. cm. Under these conditions the engine has an output of 5,580 b.h.p. The maximum output of 6,300 b.h.p. or 1,050 b.h.p. per cylinder at about 146 r.p.m. is attained with an m.e.p. of 7-4 kg./sq. cm., corresponding to a mean piston speed of 5-8 m./sec. This is the load which the engine is capable of delivering on the test bed and sea trials for a period of three hours. The rated cylinder output of 930 b.h.p. at 140 r.p.m. with an m.e.p. of 6-86 kg./sq. cm., is that for which the engine is designed on the basis of the prevailing rules of the classification societies. The recommended output for continuous service is 80 per cent to 95 per cent of the rated output, according to the actual service conditions, namely, length and severity of the voyages, the frequency and duration of harbour stops, the ambient conditions of the engine room, the quality of fuel and the state of maintenance of the engine. The Borsig-Fiat engine is exhaust turbocharged on the constant pressure series principle, the two exhaust turbochargers being of the BBC.VTR 500 type with voluted gas intakes. They are arranged ahead of the crosshead driven double acting piston scavenge pumps, the total volume of which is about 1-3 times that of the power cylinders. During the trials at the works, it was ascertained that the proportion of the compression work of the turbochargers increases with increasing engine load, while the proportion of the compression work of the engine driven scavenge pumps decreases. This characteristic is desirable from the standpoint of engine efficiency. At full load the turbochargers provide about 75 per cent of the total work required for the compression of the charging and scavenge air. Upon starting, when accelerating and in the low speed range, the piston scavenge pumps provide most of the air supply because the turbochargers do not then deliver their full capacity. In the lower speed ranges, as well as at higher speeds, the engine is readily responsive, with a smoke free exhaust. Detailed results of the tests of the 4,750-b.h.p. engine in the &#039;&#039;La Selva&#039;&#039; are shown in Fig. 2, whilst in Fig. 3 the results achieved with the engine after the further development are indicated. They show a total increase of 17-5 per cent, from 4,750 to 5,580 b.h.p., with a simultaneous rise of 130 r.p.m. to 140 r.p.m., or 7-8 per cent and a boost in b.m.e.p. from 6-3 kg. per sq. cm. to &#039;&#039;6-86&#039;&#039; kg. per sq. cm., or 9 per cent. The exhaust temperatures of the stepped-up 5,580-b.h.p. engine are 10 per cent higher whilst the charging air temperature after the blowers and before the scavenge ports, as well as the air pressure before the latter, have fallen slightly in spite of the increased boost. The ignition pressure of 65 kg. per sq. cm. when running on Diesel oil (60 kg. per sq. cm. when burning heavy fuel) remains the same. These improvements were rendered possible through higher efficiencies of the turbochargers, and improved adaptation of these blowers to the engine’s operating conditions. This also explains, for the most part, the reduction in specific fuel consumption from 164 gr. per b.h.p. per hr. to 156 gr. per b.h.p. per hr. or 4-7 per cent.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, May 1959; Vol. 40, pp. 86-87.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 24,000-b.H.p. Diesel Plant for Supertanker ==&lt;br /&gt;
[[File:1959 MAN 24000 BHP Diesel plant.png|alt=(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.|thumb|&#039;&#039;(1959) Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&#039;&#039;]]&lt;br /&gt;
In conjunction with a shipbuilding concern and a shipping company, the M.A.N. have put forward plans for the propulsion machinery of 24,000 b.h.p. for a supertanker. The four engines are of standard M.A.N. two-stroke type with 25 per cent turbocharging, the cylinders having a diameter of 570 mm. and a piston stroke of 800 mm. The speed is 225 r.p.m. The installation comprises two engines each of 7,300 b.h.p. driving a single shaft through hydraulic or electromagnetic couplings, and two engines of 6,000 b.h.p. in the wings and on a platform above the engine room floor, each driving an alternator supplying current to two 5,400-b.h.p. electric motors driving the same shaft through gearing. &lt;br /&gt;
&lt;br /&gt;
The total service output is 24,000 b.h.p. Current for the auxiliaries and for other ship requirements at sea is taken from the Diesel alternators so that no other Diesel generating plant is needed when under way. The four vertical cargo pumps are electrically driven, the electric motors being installed in the engine room. There are two Diesel generating sets for harbour and emergency duties and one gas turbine driven generator. The plant is installed in an engine room of the same size as that required for steam turbine and boiler plant. The fuel consumption is not as favourable as with the slower running, direct coupled units, the additional expenditure being about 10 gr./b.h.p.-hr., but it is considered that the saving compared with steam turbine plant is so great that this factor is not of importance.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, April 1959; Vol. 40, p. 51.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=File:1959_MAN_24000_BHP_Diesel_plant.png&amp;diff=865</id>
		<title>File:1959 MAN 24000 BHP Diesel plant.png</title>
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		<updated>2026-03-28T12:25:38Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
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&lt;div&gt;Plans of 24,000-b.h.p. machinery installation for the proposed tanker.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
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&lt;div&gt;Borsig-Fiat 1959 Fig . 3—Characteristics of the Borsig-Fiat engine when rated at 5,580 b.h.p. with a b.m.e.p. of 6-86 kg. per sq. cm.&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>File:1959 Borsig Fiat Fig 2.png</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
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&lt;div&gt;1959 Borsig Fiat Fig 2&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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	<entry>
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		<title>Engineering Abstracts 1959</title>
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		<updated>2026-03-28T11:40:19Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: /* Pressure-charged Engines */&lt;/p&gt;
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&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder Doxford type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd. The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with Burmeister and Wain main engines. The installation, which has been built by Stothert and Pitt, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by Renold’s chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency. There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr. The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure. Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “Bolnes” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the Graviner Manufacturing Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. Ruston and Hornsby, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of lOjin., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Propulsion System for Boats ==&lt;br /&gt;
[[File:1959 Propulsion System for Boats.png|alt=(1959) British Patent No. 815,182|left|thumb|374x374px|(1959) &#039;&#039;British Patent No. 815,182&#039;&#039;]]&lt;br /&gt;
This invention relates to an engine mounted inboard of the&lt;br /&gt;
&lt;br /&gt;
boat which drives a screw propeller so mounted on a support&lt;br /&gt;
&lt;br /&gt;
that the axis of the propeller is movable relative to the fore&lt;br /&gt;
&lt;br /&gt;
and aft axis of the boat for steering, the support itself being&lt;br /&gt;
&lt;br /&gt;
pivotable about a horizontal axis to lift the screw propeller&lt;br /&gt;
&lt;br /&gt;
clear of the water. In Fig. 1 the engine shaft extends in a&lt;br /&gt;
&lt;br /&gt;
fore and aft direction into the lower part of the chain case (36)&lt;br /&gt;
&lt;br /&gt;
to carry a chain sprocket (44). The shaft (29) which extends&lt;br /&gt;
&lt;br /&gt;
through the arm (15) of the L-shaped member carries another chain sprocket (45); this sprocket, when the L-shaped member&lt;br /&gt;
&lt;br /&gt;
lies within the chain case in the same plane as the sprocket&lt;br /&gt;
&lt;br /&gt;
(44) being adjacent with the upper end of the chain case. A&lt;br /&gt;
&lt;br /&gt;
sprocket chain (46) runs over the two sprockets. Two arms&lt;br /&gt;
&lt;br /&gt;
(47), pivotally mounted in the chain case and extending downwardly&lt;br /&gt;
&lt;br /&gt;
from their pivotal mountings, carry at their free ends&lt;br /&gt;
&lt;br /&gt;
sprockets (48) which engage the chain (46) inside its loop&lt;br /&gt;
&lt;br /&gt;
between the sprockets (44 and 45), the arms (47) being acted&lt;br /&gt;
&lt;br /&gt;
on by springs (49). The latter tend to urge the arms upwardly&lt;br /&gt;
&lt;br /&gt;
and outwardly. The upward and outward movement of the&lt;br /&gt;
&lt;br /&gt;
arms (47) is limited by stops (50) so as to ensure that they&lt;br /&gt;
&lt;br /&gt;
move through equal distances. It will be apparent that the&lt;br /&gt;
&lt;br /&gt;
propeller (26) can be lifted out of the water by rocking the&lt;br /&gt;
&lt;br /&gt;
L-shaped member (15, 16) rearwardly and upwardly about&lt;br /&gt;
&lt;br /&gt;
the trunnions (17) and such rocking movement will cause the&lt;br /&gt;
&lt;br /&gt;
sprocket (45) to swing downwardly and rearwardly. The upper&lt;br /&gt;
&lt;br /&gt;
part of the chain loop will tend to move downwardly with the&lt;br /&gt;
&lt;br /&gt;
sprocket (45) introducing slack in the chain (46) which will&lt;br /&gt;
&lt;br /&gt;
be taken up by upward movement of the idler sprockets (48).&lt;br /&gt;
&lt;br /&gt;
Ultimately, when the upper part of the chain (46) extends in&lt;br /&gt;
&lt;br /&gt;
a substantially straight line between the sprockets (48), as indidated&lt;br /&gt;
&lt;br /&gt;
in dotted lines in Fig. 2, the sprocket (45) will move away&lt;br /&gt;
&lt;br /&gt;
from the chain and the driving connexion between the engine&lt;br /&gt;
&lt;br /&gt;
and the propeller will be broken.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Patent No. 815,182, issued to E. J. Clerk. Complete specification published 17th June 1959.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=File:1959_Propulsion_System_for_Boats.png&amp;diff=861</id>
		<title>File:1959 Propulsion System for Boats.png</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=File:1959_Propulsion_System_for_Boats.png&amp;diff=861"/>
		<updated>2026-03-28T11:39:17Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;Drive system for boats&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=860</id>
		<title>Engineering Abstracts 1959</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=860"/>
		<updated>2026-03-28T11:36:42Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: /* Dutch V-Type Two-stroke Diesel Engine */&lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder Doxford type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd. The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with Burmeister and Wain main engines. The installation, which has been built by Stothert and Pitt, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by Renold’s chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency. There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr. The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure. Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “Bolnes” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
== Location of Temperature Rise in Engine Crankcases ==&lt;br /&gt;
A sensitive instrument for detecting temperature rise in any of the main bearing and main working surfaces within the crankcases of Diesel or petrol engines has been developed by the Graviner Manufacturing Co., Ltd. &lt;br /&gt;
&lt;br /&gt;
The apparatus is suitable for installation on all types of Diesel and petrol engines up to 500 h.p. per cylinder, either supercharged or normally aspirated, whether direct or remote-controlled, up to a maximum of 3,000 h.p. The detector is highly suitable for use on auxiliary generators or on the main propulsion engines of smaller vessels. An advantage is that a warning signal may be located, if necessary, away from the apparatus in the engine room, so that it can be ranged alongside other remote control equipment, for example in the wheelhouse. &lt;br /&gt;
&lt;br /&gt;
The Graviner detector operates on the principle of measuring the density of oil mist drawn continuously through two separate tubes of precisely similar dimensions. A beam of light projected down the axis of both tubes energizes two photo-electric cells located at the ends of the tubes from the common light source. The electrical output from each photo-electric cell is proportional to the density of light falling on the surface of each cell and, as their output is opposed electrically, no current flows when the oil mist column contained in the tubes is of equal density.&lt;br /&gt;
&lt;br /&gt;
However, when a difference occurs in the density of the mist contained in one tube relative to the other, the light beam in that tube becomes more obscured and, consequently, the system becomes electrically out of balance. An electric current then flows and operates a sensitive relay which in turn causes an audible and visible warning to occur when the differential e.m.f. reaches an optimum value. The ability of the detector to measure the extremely small quantity of oil mist associated with a corresponding rise in temperature, provides a continuous safeguard against any mechanical trouble which might arise from oil starvation or dilution; in fact, from any set of circumstances which, if allowed to continue, would utimately lead to a major breakdown. This means that apart from the detection of overheated rotating or reciprocating engine components, the high sensitivity detector will quickly sense a broken piston ring. &lt;br /&gt;
&lt;br /&gt;
Furthermore, the extreme sensitivity of the apparatus provides positive protection against crankcase explosion by warning against generation of a dangerous concentration of oil mist within the crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 8th April 1959; Vol. 140, p. 362.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pressure-charged Engines ==&lt;br /&gt;
Two medium speed Diesel engines in the VCB range manufactured by Messrs. Ruston and Hornsby, Ltd., of Lincoln, have recently been pressure charged and are now known as class VCBX engines. Available in five and six-cylinder sizes, these 5 and 6VCBX engines have a bore of 8in. and a stroke of lOjin., providing a power range of 255 to 330 b.h.p. (B.S. rating) at speeds of 600/650 r.p.m. Based on the well proved VCB engine, and incorporating an exhaust turbocharger, the up-rated engines extend the overall power range of the VCB class to 350 b.h.p., giving a total coverage of 102 to 330 b.h.p. in six engine sizes of the same cylinder dimensions, with a wide measure of interchangeability of components between the normally aspirated and pressure charged engines. &lt;br /&gt;
&lt;br /&gt;
The pressure charger employed consists of a single-stage centrifugal blower driven by an exhaust gas turbine and is air cooled. Mounted on the exhaust side of the engine, the pressure charger is lubricated from the main engine lubricating oil system. Apart from embodying a turbocharger, and the arrangement of the piston and camshaft to suit the timing of a pressure charged engine, the VCBX class is the same as the VCB engines, which enables complete component interchangeability to be maintained. As well as providing an extended power range in six engine sizes, with interchangeable components, the pressure charged units enable a lighter power unit to be installed where weight is an important factor. The pressure charged engine weighs little more than the equivalent size normally aspirated engine, giving a most favourable power/weight ratio for an engine of its type. The 5VCBX weighs 6 tons, and the 6VCBX, 7 tons. The class VCBX pressure charged engines are also suitable for marine propulsion or for auxiliary duties and are designated VCBXM and VCBXZ. The basic details of these types are given in Tables I and II.&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table I— VCBXM M arine Propulsion Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXM&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXM&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum service HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|256&lt;br /&gt;
|307&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|238&lt;br /&gt;
|285&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Maximum continous HP at gearbox &lt;br /&gt;
output coupling&lt;br /&gt;
|650&lt;br /&gt;
|230&lt;br /&gt;
|277&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|213&lt;br /&gt;
|256&lt;br /&gt;
|}&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&#039;&#039;&#039;Table&#039;&#039;&#039; II—&#039;&#039;&#039;VCBXZ M arine Auxiliary Engines&#039;&#039;&#039;&lt;br /&gt;
!&#039;&#039;Engine&#039;&#039;&lt;br /&gt;
!RPM&lt;br /&gt;
!&#039;&#039;5VCBXZ&#039;&#039;&lt;br /&gt;
!&#039;&#039;6VCBXZ&#039;&#039;&lt;br /&gt;
|-&lt;br /&gt;
| rowspan=&amp;quot;2&amp;quot; |Continous Service HP&lt;br /&gt;
|650&lt;br /&gt;
|276&lt;br /&gt;
|330&lt;br /&gt;
|-&lt;br /&gt;
|600&lt;br /&gt;
|255&lt;br /&gt;
|306&lt;br /&gt;
|}&lt;br /&gt;
&#039;&#039;—The Shipbuilder and Marine Engine-Builder, February 1959; Vol. 66, p. 113.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
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		<title>Engineering Abstracts 1959</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: /* Oil Motor Pump Drive */&lt;/p&gt;
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&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
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= Engineering Abstracts from 1959 =&lt;br /&gt;
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== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
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The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
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For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
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In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
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As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
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—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
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== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
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advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
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—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
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== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
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—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
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== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
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&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
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== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
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—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
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== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
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—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
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== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
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—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
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== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
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—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
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== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
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—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
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== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
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—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
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== Oil Motor Pump Drive ==&lt;br /&gt;
[[File:1959 Oil Motor Pump Drive.png|alt=General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive acting, screw displacemetit pump of their unidirectional flow design|thumb|&#039;&#039;General arrangement of hydraulically driven pumps. The generator pump is chain driven from the propeller shaft and is a Stothert and Pitt positive  acting, screw displacemetit pump of their unidirectional flow design.&#039;&#039;]]&lt;br /&gt;
A set of engine cooling and lubricating pumps driven hydraulically from the main engine are to be installed in the oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039; &#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder Doxford type Diesel engine and the hydraulic installation is being supplied and has been developed by Stothert and Pitt, Ltd. The use of hydraulically driven salt and fresh water cooling pumps has previously been largely confined to Danish-built vessels, and the system has been installed in a number of vessels fitted with Burmeister and Wain main engines. The installation, which has been built by Stothert and Pitt, Ltd., consists of a generator pump, a motor pump, a salt water pump and a fresh water pump. The generator pump will be located alongside the propeller shaft and will be driven by Renold’s chains through a step-up gearbox. The direct drive arrangement offers a considerable saving in fuel by taking the load off the ship’s generators. The additional fuel consumed by the main engine is a good deal less than what would have been used in the auxiliary set, due to the higher efficiency. There is also the benefit of simplicity with the direct drive arrangement. The arrangement of the installation is shown on the accompanying drawing. The generator unit consists of a Stothert and Pitt horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing gears, and fitted with mechanical seals. The pump body is split and a pilot operated pressure relief valve with an external exhaust  flange is fitted. The speed of the pump is 745 r.p.m. with a discharge pressure of about 3001b. per sq. in., the output being 250 tons per hr. The motor pump is an S. and P. horizontal, positive acting, screw displacement pump having internal bearings and timing gears, with shafts extended at each end for coupling to the water pumps. The suction and delivery branches are in the bottom half of the body, which is split through its centre line, the pump covers being designed to withstand 601b. per sq. in. working pressure. Two mechanical seals are fitted and the pump is equipped with a relief valve having an external flange for returning oil back to source. This pump receives oil from the generator at approximately 300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b. per sq. in. at a rate of 250 tons per hr. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
[[File:1959 Bolnes Two stroke V diesel.png|alt=1959 Bolnes Diesel Engine in V form|left|thumb|312x312px|1959 Bolnes Diesel Engine in V form]]&lt;br /&gt;
The N.V. Machinefabriek “Bolnes” v.h. J. H. van Capellen has developed a V-built two-stroke Diesel engine available in both naturally-aspirated and turbocharged types and in units from six to twenty cylinders. The first engine, a 1,000-h.p. unit, will be placed in the suction dredger &#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V., where it will drive the sand pump. The new V-built Bolnes engine is constructed in accordance with the standardized system adopted by the builders after the war and which makes use of welded construction on a large scale and of 50-h.p. units enabling the construction of in-line engines ranging between 100 and 500 h.p., that is, two to ten cylinders. For larger outputs twin sets are available. The V-built engine is available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin arrangement enables outputs of up to 3,000 h.p. Like the in-line type of engine, the V-built version is of the crosshead type which uses the cylindrical crosshead and guide as a reciprocating scavenge pump. Uniflow scavenging is employed and circulation cooling is achieved by a pipe cooler. The fuel consumption is 170 grammes per h.p. per hr. and lubricating oil consumption 0’8 grammes per h.p. per hr. The bore is 190 mm. and the stroke 350 mm. The engine has an all-welded single-piece frame with box-type girders. The front columns are of steel and can be taken away for the removal of the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=File:1959_Bolnes_Two_stroke_V_diesel.png&amp;diff=858</id>
		<title>File:1959 Bolnes Two stroke V diesel.png</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=File:1959_Bolnes_Two_stroke_V_diesel.png&amp;diff=858"/>
		<updated>2026-03-28T11:24:59Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;Bolnes V engine - diesel&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=File:1959_Oil_Motor_Pump_Drive.png&amp;diff=857</id>
		<title>File:1959 Oil Motor Pump Drive.png</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=File:1959_Oil_Motor_Pump_Drive.png&amp;diff=857"/>
		<updated>2026-03-28T11:21:09Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;Illustration 1959 Oil Motor Pump Drive&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=856</id>
		<title>Engineering Abstracts 1959</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=856"/>
		<updated>2026-03-28T08:23:03Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Oil Motor Pump Drive ==&lt;br /&gt;
A set of engine cooling and lubricating pumps driven&lt;br /&gt;
&lt;br /&gt;
hydraulically from the main engine are to be installed in the&lt;br /&gt;
&lt;br /&gt;
oil tanker &#039;&#039;Regent Eagle,&#039;&#039; 19,000 tons d.w., now under construction&lt;br /&gt;
&lt;br /&gt;
by the Blythswood Shipbuilding Co., Ltd. The &#039;&#039;Regent&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;Eagle&#039;&#039; will be powered by a six-cylinder Doxford type Diesel&lt;br /&gt;
&lt;br /&gt;
engine and the hydraulic installation is being supplied and has&lt;br /&gt;
&lt;br /&gt;
been developed by Stothert and Pitt, Ltd. The use of&lt;br /&gt;
&lt;br /&gt;
hydraulically driven salt and fresh water cooling pumps has&lt;br /&gt;
&lt;br /&gt;
previously been largely confined to Danish-built vessels, and&lt;br /&gt;
&lt;br /&gt;
the system has been installed in a number of vessels fitted with&lt;br /&gt;
&lt;br /&gt;
Burmeister and Wain main engines. The installation, which&lt;br /&gt;
&lt;br /&gt;
has been built by Stothert and Pitt, Ltd., consists of a generator&lt;br /&gt;
&lt;br /&gt;
pump, a motor pump, a salt water pump and a fresh water&lt;br /&gt;
&lt;br /&gt;
pump. The generator pump will be located alongside the&lt;br /&gt;
&lt;br /&gt;
propeller shaft and will be driven by Renold’s chains&lt;br /&gt;
&lt;br /&gt;
through a step-up gearbox. The direct drive arrangement offers&lt;br /&gt;
&lt;br /&gt;
a considerable saving in fuel by taking the load off the ship’s&lt;br /&gt;
&lt;br /&gt;
generators. The additional fuel consumed by the main engine&lt;br /&gt;
&lt;br /&gt;
is a good deal less than what would have been used in the&lt;br /&gt;
&lt;br /&gt;
auxiliary set, due to the higher efficiency. There is also the&lt;br /&gt;
&lt;br /&gt;
benefit of simplicity with the direct drive arrangement. The&lt;br /&gt;
&lt;br /&gt;
arrangement of the installation is shown on the accompanying&lt;br /&gt;
&lt;br /&gt;
drawing. The generator unit consists of a Stothert and Pitt&lt;br /&gt;
&lt;br /&gt;
horizontal, positive acting, screw displacement pump of their unidirectional flow design, having internal bearings and timing&lt;br /&gt;
&lt;br /&gt;
gears, and fitted with mechanical seals. The pump body is&lt;br /&gt;
&lt;br /&gt;
split and a pilot operated pressure relief valve with an external&lt;br /&gt;
&lt;br /&gt;
exhaust flange is fitted. The speed of the pump is 745 r.p.m.&lt;br /&gt;
&lt;br /&gt;
with a discharge pressure of about 3001b. per sq. in., the&lt;br /&gt;
&lt;br /&gt;
output being 250 tons per hr. The motor pump is an S. and&lt;br /&gt;
&lt;br /&gt;
P. horizontal, positive acting, screw displacement pump having&lt;br /&gt;
&lt;br /&gt;
internal bearings and timing gears, with shafts extended at each&lt;br /&gt;
&lt;br /&gt;
end for coupling to the water pumps. The suction and&lt;br /&gt;
&lt;br /&gt;
delivery branches are in the bottom half of the body, which is&lt;br /&gt;
&lt;br /&gt;
split through its centre line, the pump covers being designed&lt;br /&gt;
&lt;br /&gt;
to withstand 601b. per sq. in. working pressure. Two&lt;br /&gt;
&lt;br /&gt;
mechanical seals are fitted and the pump is equipped with a&lt;br /&gt;
&lt;br /&gt;
relief valve having an external flange for returning oil back to&lt;br /&gt;
&lt;br /&gt;
source. This pump receives oil from the generator at approximately&lt;br /&gt;
&lt;br /&gt;
300 lb. per sq. in. and delivers it at 1,450 r.p.m. at 601b.&lt;br /&gt;
&lt;br /&gt;
per sq. in. at a rate of 250 tons per hr.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 29th April 1959; Vol. 140, p. 437.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Dutch V-Type Two-stroke Diesel Engine ==&lt;br /&gt;
The N.V. Machinefabriek “Bolnes” v.h. J. H. van&lt;br /&gt;
&lt;br /&gt;
Capellen has developed a V-built two-stroke Diesel engine&lt;br /&gt;
&lt;br /&gt;
available in both naturally-aspirated and turbocharged types and&lt;br /&gt;
&lt;br /&gt;
in units from six to twenty cylinders. The first engine, a&lt;br /&gt;
&lt;br /&gt;
1,000-h.p. unit, will be placed in the suction dredger&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;Vlaardingen,&#039;&#039; under construction for Adriaan Volker, N.V.,&lt;br /&gt;
&lt;br /&gt;
where it will drive the sand pump. The new V-built Bolnes&lt;br /&gt;
&lt;br /&gt;
engine is constructed in accordance with the standardized&lt;br /&gt;
&lt;br /&gt;
system adopted by the builders after the war and which makes&lt;br /&gt;
&lt;br /&gt;
use of welded construction on a large scale and of 50-h.p.&lt;br /&gt;
&lt;br /&gt;
units enabling the construction of in-line engines ranging&lt;br /&gt;
&lt;br /&gt;
between 100 and 500 h.p., that is, two to ten cylinders. For&lt;br /&gt;
&lt;br /&gt;
larger outputs twin sets are available. The V-built engine is&lt;br /&gt;
&lt;br /&gt;
available in six to twenty cylinder units up to a maximum output of 1,500 e.h.p. at 475 r.p.m., when supercharged. Twin&lt;br /&gt;
&lt;br /&gt;
arrangement enables outputs of up to 3,000 h.p. Like the&lt;br /&gt;
&lt;br /&gt;
in-line type of engine, the V-built version is of the crosshead&lt;br /&gt;
&lt;br /&gt;
type which uses the cylindrical crosshead and guide as a reciprocating&lt;br /&gt;
&lt;br /&gt;
scavenge pump. Uniflow scavenging is employed&lt;br /&gt;
&lt;br /&gt;
and circulation cooling is achieved by a pipe cooler. The fuel&lt;br /&gt;
&lt;br /&gt;
consumption is 170 grammes per h.p. per hr. and lubricating&lt;br /&gt;
&lt;br /&gt;
oil consumption 0’8 grammes per h.p. per hr. The bore is&lt;br /&gt;
&lt;br /&gt;
190 mm. and the stroke 350 mm. The engine has an&lt;br /&gt;
&lt;br /&gt;
all-welded single-piece frame with box-type girders. The front&lt;br /&gt;
&lt;br /&gt;
columns are of steel and can be taken away for the removal of&lt;br /&gt;
&lt;br /&gt;
the built-up crankshaft.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Holland Shipbuilding, January 1959; Vol. 7, p. 30.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
	</entry>
	<entry>
		<id>https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=855</id>
		<title>Engineering Abstracts 1959</title>
		<link rel="alternate" type="text/html" href="https://wiki.oldengin.es/index.php?title=Engineering_Abstracts_1959&amp;diff=855"/>
		<updated>2026-03-27T20:29:10Z</updated>

		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
&lt;br /&gt;
= Engineering Abstracts from 1959 =&lt;br /&gt;
&lt;br /&gt;
== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== The Stork Marine Diesel Engine ==&lt;br /&gt;
The Stork marine Diesel engine is a single acting two-stroke engine, with uniflow scavenging by means of scavenging ports in the cylinder liner, and four poppet exhaust valves in the cylinder cover. This type of engine is particularly suitable for turbocharging by means of exhaust gas driven turboblowers and so the majority of these engines are now ordered turbocharged. The last normally aspirated engine ordered was delivered last year. There are now three standard sizes of this engine, namely: —&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|+&lt;br /&gt;
!&lt;br /&gt;
!Bore&lt;br /&gt;
mm&lt;br /&gt;
!Stroke &lt;br /&gt;
mm&lt;br /&gt;
!Output per cylinder&lt;br /&gt;
|-&lt;br /&gt;
|Small&lt;br /&gt;
|540&lt;br /&gt;
|1150&lt;br /&gt;
|500 - 520 b.h.p. at 135 - 145 r.p.m.&lt;br /&gt;
|-&lt;br /&gt;
|Medium&lt;br /&gt;
|630&lt;br /&gt;
|1350&lt;br /&gt;
|800 bhp. at 132 rpm&lt;br /&gt;
|-&lt;br /&gt;
|Large&lt;br /&gt;
|750&lt;br /&gt;
|1500 - 1600&lt;br /&gt;
|1200 - 1300 bhp at 115 - 118 rpm&lt;br /&gt;
|}&lt;br /&gt;
This range thus covers outputs from 2,500 b.h.p. in five cylinders of 540-mm. bore up to about 15,000 b.h.p. in 12 cylinders of 750-mm. bore, all turbocharged. Normally aspirated engines of the small bore, but with a stroke of 900 mm. have been delivered for an output of 375 b.h.p. per cylinder at 155 r.p.m., whereas for ratings above 15,000 b.h.p. a new size of 850-mm. bore is being developed for an output of 20,000 b.h.p. in 12 cylinders. The engine frame is a rigid assembly of bedplate, columns and cylinder blocks, vertically connected by long tie bolts from the top of the cylinder block to the lower part of the bedplate. The tie bolts are tightened hydraulically and arranged to take the combustion forces and thus  relieve the frame of tensile stresses. The jerk type fuel pumps, one for each cylinder, are mounted over the camshaft as near as possible to their relative cylinder covers, thus allowing high pressure fuel lines of minimum length, which is important for the use of residual fuel. The fuel pump is operated from the fuel cam in the normal way by means of a roller cam follower in a roller holder. The pump plunger is lapped in a case hardened steel barrel, both easily renewable. The pump is provided with a suction and delivery valve; fuel delivery is controlled at the end of the pump stroke by mechanical lifting of the suction valve by means of a gear with levers and push rods, actuated by the roller holder. The fuel delivery is regulated by one of these levers pivoting on an eccentric control shaft. As the suction valve has to be opened against injection pressure, it is provided with a small pilot valve, opening 0&#039;5 mm. prior to the main valve and thus efficiently releasing the pump pressure and so decreasing the load on the control gear. The delivery valve is provided with a built-in release valve, opening at a pressure difference of 100 kg. per sq. cm. between the h.p. fuel line and pump chamber, thus ensuring immediate pressure release in the h.p. fuel line at the end of the pump delivery and so preventing any risk of after-dripping of the fuel valve. The fuel valve is of the normal needle valve type, which is spring loaded and opened by the fuel pressure. The engine is reversed by means of starting air, operating a reversing piston. The reversing piston effects the turning of a reversing shaft, running parallel to the camshaft, which moves the cam followers free from the cams prior to the axial displacement of the camshaft, which is also effected by the reversing piston. The engine is turbocharged by means of exhaust driven turboblowers (of the gas entry type); they are entirely self-regulating. The pulse system of turbocharging is used, which means that the turbine energy is derived from the kinetic energy of the exhaust gases (speed) in addition to their static energy (pressure and temperature). Maximum perfection of this system has been attained by the use of one turbocharger for two adjacent cylinders and by arranging them at cylinder head level to achieve the smallest possible volume of exhaust piping between the cylinder cover and exhaust turbine. As, moreover, a rapid release of the exhaust gases is of paramount importance for this system, four exhaust valves have been provided for each cylinder. The exhaust pulse diagram, Fig. 12, clearly demonstrates the importance of the exhaust pulse energy in comparison with the static energy and also the possibility of a high exhaust peak pressure during pre-exhaustion in combination with a sufficiently low exhaust pressure to ensure efficient scavenging of the cylinder. The diagram also shows the requirement of a crank angle difference of at least 120 degrees between the cylinders which are connected to a common turbocharger in order to avoid the exhaust pulse of one cylinder disturbing the scavenging process of the other. This requirement can be satisfied by a crank sequence combining satisfactory engine balance with normal torsional vibration characteristics.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by A. Hootsen and E. A. van der Molen, read at a meeting of the Institution of Engineers and Shipbuilders in Scotland on 24th February 1959.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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		<title>Engineering Abstracts 1959</title>
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		<summary type="html">&lt;p&gt;Toro Andersen: &lt;/p&gt;
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&lt;div&gt;[[Engineering Abstracts|Back to the index of Engineering Abstracts]]&lt;br /&gt;
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= Engineering Abstracts from 1959 =&lt;br /&gt;
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== Project for the Machinery of a 65,000-ton Nuclear Tanker ==&lt;br /&gt;
A first design of a nuclear powered ship was made at Gotaverken Shipyard during the autumn and winter of 1956. The purpose was primarily to obtain a subject for further discussions, detailed investigations and calculations. The project was intended for a tanker of 65,000 tons d.w. with a machinery power of 30,000 s.h.p., and the reactor was of the boiling water type with the steam formed in the core and fed directly to the turbines. &lt;br /&gt;
&lt;br /&gt;
The main propulsion machinery should at normal load produce 30,000 s.h.p. divided between two propellers. This gives a trial speed of 18,25 knots, and a corresponding speed in service of about 17,75 knots. The power transmission from the turbine to the propeller shaft should be electrical &#039;&#039;via&#039;&#039; two independent turbogenerators with 11,7 MW coupling power each and two propeller motors with a shaft power of 15,000 s.h.p. each. For propulsion in passages, where the reactor is forbidden to operate, there are two high speed Diesel alternators of 2,000 kW, which are expected to give the ship a speed of about 9 knots. &lt;br /&gt;
&lt;br /&gt;
For production of all auxiliary power needed there are 6 Diesel alternators, each of 400 kW. These are running the pumps of the reactor, the pumps and exciters of the turbogenerators and the rest of the auxiliary machinery on the ship. Two oil fired header type boilers, with a total capacity of 34 tons of steam per hr. of 1701b. per sq. in. gauge are supplying heat to the heating coils, etc. The machinery is located in two engine rooms, one amidship and one aft. In the midship space the reactor with its pumps and the main turbogenerators with their condensers, pumps, etc., are placed. In the aft room are located the propeller motors, the auxiliary Diesel engine, the emergency Diesel engines, the steam boilers and all other conventional equipment. The reactor control room is situated in connexion with the aft engine room. The equipment for water purification, etc., for the primary system is located in a deck house above the midship engine room. With the arrangement described above, several advantages are obtained. Thus, there will be a complete separation of those spaces which are containing radioactive material or might be filled with radioactive material in connexion with a failure or an accident, and those spaces which people normally occupy, i.e. cabins, bridge and the remaining part of the machinery. &lt;br /&gt;
&lt;br /&gt;
In the first mentioned spaces admittance will not be allowed during reactor operation. The reactor is normally producing 132 tons of saturated steam per hour at a pressure of 5851b. per sq. in. gauge, corresponding to a thermal power of 100 MW. Four circulating pumps, located inside the primary shield, provided a 30-fold circulation of the reactor water. The fuel elements are made up of plates of uranium metal canned in Zircaloy. The large cooling area means that the demands upon the purity of the water need not be exaggerated and the materials in the plant might be of normal quality.&lt;br /&gt;
&lt;br /&gt;
As nobody is allowed to enter the midship space where the reactor is located during operation, the primary shield around the reactor can be of relatively small weight, about 750 tons, instead of normally 1,000 tons. However, 20 minutes after shut down the reactor space might be occupied for an unlimited time without any risk of over exposure. In respect of weight a boiling water reactor is particularly favourable; as the pressure vessel is relatively light, a “pressurizer” is not needed, and there are no heat exchangers. The total machinery weight will therefore not exceed that of a Diesel or turbine plant with more than 500-1,500 tons. The nuclear ship has accordingly a greater real loading capacity even on the Suez route, and on the Cape route the loading capacity is 10 per cent greater than that of a conventional steamship. In this case the cost per ton loading capacity is almost the same as that of a steamship. A comparison with a Diesel ship, however, turns out more unfavourable.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;L. Nordstrom and J. Thunell, International Shipbuilding Progress, August 1958; Vol. 5, pp. 365-376.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== German Multi-engine Propulsion Proposal ==&lt;br /&gt;
[[File:1959 MAN K9Z57-80.png|alt=M.A.N. design for combined geared Diesel and Diesel electric drive of 24,500 b.h.p.|left|thumb|279x279px|&#039;&#039;M.A.N. design for combined geared Diesel and Diesel electric&#039;&#039; ]]&lt;br /&gt;
An unusual design for ship propelling machinery developing 24,500 s.h.p. on a single shaft has been prepared by Maschinenfabrik Augsburg-Nurnberg A.G. in close cooperation with shipyards and tanker owners. The use of multiple engine propulsion has been advocated for a number of years, and examples of this form of propulsion will be found in a large number of ships. As an alternative to the direct coupled engine, the geared Diesel engine is the most satisfactory form of indirect drive, for it offers several&lt;br /&gt;
&lt;br /&gt;
advantages to the prospective user. These include: a saving in space; increased reliability, as there is very little chance of all engines breaking down at once; the ability to overhaul the engines while at sea; and the advantage that for economical reasons one or more of the engines can be shut down when the ship is light. The project prepared by M.A.N. is unusual because it is a combination of geared Diesel and Diesel-electric drive. The weight of the complete installation including Diesel engines, gears and couplings, electric generators  and motors, without the auxiliary equipment, is about 1,240 tons. The entire machinery can be accommodated in the same amount of space as that required for a turbine installation of similar capacity, without having to extend the hull. The installation consists of two M.A.N. engines, each of 7,000 b.h.p., coupled to the shaft through electro-magnetic couplings or hydraulic couplings and gearing; and two 6,000-b.h.p. engines on flats above and to the side, each driving an alternator which supplies current to electric motors coupled to the main gearbox. With this system, various combinations of drive may be obtained, each having different economic advantages, depending on the amount of cargo being carried, and other circumstances. It must be admitted, however, that the fuel consumption of this proposed scheme would be about 0 0211b. per h.p. higher than that of a slow running engine. For one reason the fuel consumption of the high speed engine is higher because of its slightly lower efficiency, and for another the gearing losses and electrical transmission losses must be taken into consideration. The M.A.N. engines used for the scheme would be suitable for operation on heavy fuel, and would be of the crosshead design with complete separation of cylinder block and crankcase.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipping World, 24th September 1958; Vol. 139, p. 283.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Pielstick-engined Passenger Vessel with Alternative Speeds ==&lt;br /&gt;
The keel was laid last month at the Forges et Ch. de la Mediterranee, La Seyne, of an unusual passenger vessel being built for the Cie. Generale Transatlantique, to be operated,  according to season, either on the Nice-Corsica or the Marseilles-Corsica service. She is a ship of 4,500 gross tons, to be equipped with 8,000 b.h.p. Pielstick machinery and will have a service speed of 18 knots or 14½ knots, according to the requirements, namely, whether on the Nice or Marseilles run. The four 2,000-b.h.p. SEMT-Pielstick engines are coupled to two shafts through an ASEA electro-magnetic clutch, and with two engines in operation the lower speed of 14½ knots will be easily maintained. The length b.p. is 326ft. 5in., the moulded breadth 51 ft. 10 in. and the maximum draught 15ft. 7in. The deadweight is 1,000 tons and in addition to accommodation for 114 first class, 224 second class and 700 third class passengers, 80 motor cars can be carried, of which 44 will be accommodated in a closed garage. The name of the ship will be &#039;&#039;Napoleon.&#039;&#039; &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== 15,000-s.h.p. 26,700-ton Soviet Whale Factory Ship ==&lt;br /&gt;
Details are now available of the first large whale factory ship to be built in Russia. She is under construction at the Nikolaiev yard and is named &#039;&#039;Sovietskaya Ukraina.&#039;&#039; The displacement will be 44,000 tons, the length overall 217,8 m., the breadth 27,8 m. and the loaded draught 10,6 m. She is propelled by two 7,500-b.h.p. Burmeister and Wain six-cylinder turbocharged units running at 115 r.p.m. and the speed will be 16 knots. For the supply of current, four 750-kW Diesel engined generators are installed. The crew and factory workers will total 487 men. A helicopter will be carried on deck. To operate with the factory ship there will be a number of 18-knot whalers constructed, also at Nikolaiev, each 63-6 m. in overall length with a breadth of 9-5 m. and a draught of 4-41 m. Diesel electric machinery of 3,100 b.h.p. is to be installed in each ship and they could operate for 25 days without refuelling.&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;—The Motor Ship, November 1958; Vol. 39, p. 374.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Notes on the Jerk System of Fuel Injection ==&lt;br /&gt;
The paper aims at drawing attention to certain features of the injection of fuel into the cylinders of compression ignition engines. It is in effect a continuation of that contributed to the Institution of Mechanical Engineers by one of the authors in 1940. Since then data have been accumulated and certain new facts have come to light. As in that paper, attention is confined to the jerk system of fuel injection employing independent pumps and injectors. The authors refer therefore in the first place to the effect on the injection process of details of the design of the nozzle valve (differential needle). They deal secondly with the effect of the elasticity of the fuel trapped between the pump delivery valve and the nozzle needle valve. From this they build up calculated indicator diagrams for the fuel delivery pipe and then arrive at figures for calculated injection period under various conditions. In these calculations consideration of pipe surges is omitted. They then go on to recommend a procedure for determining the most favourable particulars and dimensions of the fuel injection equipment in any particular engine. In the course of the paper a number of numerical calculations are made to illustrate the influence of the several variables on the injection process. They are based on certain simplifying assumptions made to reduce the calculations to manageable proportions. It is stressed therefore that the numerical results derived are indicative of trends and cannot be accepted as representing actual facts.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;Paper by W. A. Green and G. R. Green, read at the General Meeting of the Diesel Engineers and Users Association, 20th November&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Direct Bridge Control of Ships’ Engines ==&lt;br /&gt;
Direct bridge control of ships’ engines has been in operation in the United States of America, as well as several other countries, for some time. In order to obtain the maximum benefit from such a system, of course, two or more operational positions are required on the bridge or superstructure. The tug &#039;&#039;Flying Dipper,&#039;&#039; owned by the Clyde Shipping Co., Ltd., of Glasgow, and powered by a British Polar Diesel engine, is the first vessel to work in United Kingdom waters using a full application of pneumatic control equipment, and she has four operational positions on the bridge. The vessel can also be controlled direct from the engine room. Single lever control is provided at the four bridge positions and the interlock features of the controls prevent any mishandling of the engines. Westinghouse type-2A2A Controlair valves are installed at all these single lever control points. Selection of direction is made in the first movement from the neutral position and effected by passing an air signal down the ahead or astern signal line, as required. This operates a three-position cylinder mounted on the gearbox, and a pneumatic interlock connects the throttle signal line from the Controlair valve to the control port of a Pneudyne positioner mounted on the main engine. This unit is of the servo pattern and provides accurate positioning of the engine throttle in response to the signal given from the bridge. By means of a time delay feature, the engine may be opened up at a .maximum predetermined speed. A pneumatic time delay unit is built into the gearbox control system to ensure that when going from ahead to astern, or &#039;&#039;vice versa,&#039;&#039; there is a short pause in the neutral position before the new drive position is selected. To change from one control position on the bridge to another is simple. The only action required is to depress the changeover button at the new position until the air supply is registered on the air pressure gauge, mounted locally. Full control is then available at the new position. To change control between the engine room and any bridge position, the engineer operates his locally mounted Rotair valve. While the &#039;&#039;Flying Dipper&#039;&#039; is fitted with special control desks incorporating the pneumatic valves, it is claimed that the equipment is suitable for operation by a conventional ship’s telegraph head. Whaling ships, Great Lakes ore carriers, spirit tankers, bulk sugar carriers, a Canadian Shell tanker and Admiralty frigates and tugs are among the ships fitted, or being fitted, with pneumatic control equipment.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;The Shipbuilder and Marine Engine-Builder, November 1958; Vol. 65, p. 630.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Engine Noise Investigation ==&lt;br /&gt;
The demand for higher operating speed and power, combined with light weight construction, has resulted in a considerable increase in the noise level of modern naval Diesel engines. To safeguard the health of crews and to ensure that orders can be heard and understood, the Admiralty Engineering Laboratory at West Drayton, Middlesex, is devoting considerable attention to the design of efficient silencer systems. Since trials and tests of actual Diesel engines would be expensive, slow and very noisy, special laboratory techniques have been developed. One method which has given excellent results involves the use of an unusual means of noise simulation. Instead of attempting to reproduce the noise frequency spectrum of a given engine, “white” noise (of equal loudness at all frequencies) is fed into an experimental silencer, whose “exhaust” terminates in an anechoic chamber. A microphone in the chamber feeds an a.f. analyser by means of which the output noise spectrum is plotted. The extent and characteristics of the attenuation given by the model under test can thus be established, in comparison with a datum spectrum obtained by replacing the silencer with a straight pipe. &lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;British Communications and Electronics, December 1958; Vol. 5, p. 954.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Buchi Telescope-valve System on Four-cycle Diesel Engines ==&lt;br /&gt;
The telescope valve engine is an improved four-stroke&lt;br /&gt;
[[File:1959 Buchi.png|alt= |left|thumb|Fig . 2&#039;&#039;—Transverse section through a Buchi telescope valve high speed Diesel engine&#039;&#039;]]&lt;br /&gt;
cycle internal combustion engine, built with or without pressure charging, preferably combined with scavenging to sweep out the exhaust gases from and to cool the combustion space. A swirl is generated in this space for a simple and perfect fuel distribution and combustion. Such an engine design may be adopted for internal combustion engines of any size and use, and of any cylinder arrangement. The telescope valve system and its special design of the cylinder head, combustion chambers, valves, fuel injection system and valve control mechanism are *tso favourable for other than Diesel engines, such as gas, gasoline or heavy fuel engines. Two valves are provided, one coaxially arranged within the other; one of them serving for admitting the charge and the other for discharging the exhaust gases. This system, the so-called telescope or concentric valve system, by means of its concentric valves in conjunction with the form of the upper part of the piston closing the combustion chamber, in its outer dead centre position gives the combustion chamber the shape of a relatively deep disc while the valves are closed. To obtain ample flow areas relatively adjacent to the valve openings or seats, a corresponding form of the combustion space is chosen in the cylinder head and/or in the piston top. Thus, a circumferential wall is formed around the combustion chamber which conducts the intake air flowing from the inlet valve opening to that of the exhaust valve. Furthermore, the combustion chamber and the cylinder head on its inner side may be so shaped that when the piston is in T.D.C. position and both valves are open, the inner valve disc extends to a corresponding complementary portion of the piston head and an annular passage is formed between the valve disc and the adjacent walls. The valves and its discs are so shaped that the charge entering through one of the valves is led to the other valve by flowing around the outer valve disc, thereby sweeping through the whole combustion chamber. The valve bodies, the inner wall of the combustion chamber and the surface of the piston head may be given such a shape that, with both valves open, passages of smooth configuration for the scavenging air are formed which provide approximately constant stream areas. The seat of the inner valve may be recessed so deeply into the outer valve body, and the part of the inner valve body projecting into the combustion chamber is rounded to such an extent, that the scavenging air is deviated gradually and regularly from one valve opening to the other. The surface of the piston head may be advantageously so shaped as to surround, in the T.D.C. position, the surface of the projection on the exhaust valve disc in the open position of this disc. The charge either can be admitted around the outer valve and discharged through the inner annular space between the two valves or &#039;&#039;vice versa.&#039;&#039; Moreover, to the entering charge may be imparted advantageously a rotatory movement about the valve axis, by means of tangential or spiral entrance-surface portions or separate guide surfaces. Alternatively, for effecting this whirling movement the connecting ribs between the stem and the sleeve of the outer valve can be utilized, which may be provided with helical surfaces. Because of this design, the insides of the cylinder head and of the piston top surrounding the combustion space are absolutely symmetrical to the cylinder axis and have a minimum of relatively plain and regular surfaces. For a sufficient opening of both valves, even during the scavenging period, no cuts or the like are necessary in the piston head or in the cylinder liner for these valves when the piston is near or in its T.D.C. position. The fuel injector or injectors are located in such a manner that the injected fuel arrives uniformly distributed in the combustion space. The fuel injection device or devices inject the fuel in a direction which is transverse and, if necessary, also oblique to the cylinder axis.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;A. J. Buchi: paper contributed to the Oil and&#039;&#039; &#039;&#039;Gas Power Division Conference, 1958, of the American Society&#039;&#039; &#039;&#039;of Mechanical Engineers, Gas and Oil Power, December&#039;&#039; &#039;&#039;1958; Vol. 53, pp. 325-328.&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
== Cylinder Wear in Marine Diesel Engines ==&lt;br /&gt;
If in a marine Diesel engine chromium plated liners are used and if this engine runs on a fuel with a high sulphur content, a difference in potential between the cylinder wall and the piston can be measured. This potential difference is due to the existence of a galvanic cell formed by the chromium plated wall and the cast iron piston rings with an acid oil film on the wall as electrolyte. From the results on a test engine it could be calculated that an important part of the corrosive wear of the chromium plated liners is due to the action of this cell. The test engine used for these measurements was a stationary two-cylinder, single acting, two-stroke crosshead Bolnes engine with a bore of 190 mm. (Fig. 4). This medium speed engine (430 r.p.m.) with 50 h.p. per cylinder is very suitable for experiments on cylinder wear because of insensitivity to fuel quality and the completely separated cylinder lubrication. As the composition of the oil film on the cylinder wall is important in the study of cylinder wear, drip trays were fixed to the bottom of the liners with drainpipes leading outside the engine. In this way the cylinder oil that runs down from the wall could be collected at regular intervals. The samples were analysed at once on their water and sulphuric acid content. Another modification in the construction of the engine was necessary to make sure that the measured differences in potential originated indeed from the system piston cylinder. Therefore the piston has to be electrically insulated from the piston rod. It was found that as soon as the engine runs under normal conditions of speed, load and cooling water temperature, the cylinder wall is about 300-400 mV negative relative to the piston near T.D.C. and becomes positive at about 100 mm. from the top. Somewhat farther than halfway down the expansion stroke the difference in potential is negligible.&lt;br /&gt;
&lt;br /&gt;
—&#039;&#039;W. A. Schultze, International Building Progress, December 1958; Vol. 5, pp. 566-576.&#039;&#039;&lt;/div&gt;</summary>
		<author><name>Toro Andersen</name></author>
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