One of the earliest of the British-built Vee type engines was an
eight-cylinder 50 horse-power by the Wolseley Company, constructed
in 1908 with a cylinder bore of 3·75 inches and stroke of 5 inches,
running at a normal speed of 1,350 revolutions per minute. With this
engine, a gearing was introduced to enable the propeller to run at a
lower speed than that of the engine, the slight loss of efficiency
caused by the friction of the gearing being compensated by the slower
speed of the air-screw, which had higher efficiency than would have
been the case if it had been run at the engine speed. The ratio of the
gearing--that is, the speed of the air-screw relatively to that of the
engine, could be chosen so as to suit exactly the requirements of the
air-screw, and the gearing itself, on this engine, was accomplished on
the half-speed shaft actuating the valves.
Very soon after this first design had been tried out, a second Vee type
engine was produced which, at 1,200 revolutions per minute, developed
60 horse-power; the size of this engine was practically identical with
that of its forerunner, the only exception being an increase of half an
inch in the cylinder stroke--a very long stroke of piston in relation
to the bore of the cylinder. In the first of these two engines, which
was designed for airship propulsion, the weight had been about 8 lbs.
per brake horse-power, no special attempt appearing to have been made
to fine down for extreme lightness; in this 60 horse-power design, the
weight was reduced to 6·1 lbs. per horse-power, counting the latter
as normally rated; the engine actually gave a maximum of 75 brake
horse-power, reducing the ratio of weight to power very considerably
below the figure given.
[Illustration: Sikh, 12-cylinder magneto, end view.]
[Illustration: Sikh, 12-cylinder, side view.]
Public-domain text, read in full here on John Shaqi.
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