Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911Langley, S. P. (Samuel Pierpont)
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Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911
Langley, S. P. (Samuel Pierpont)
Aeronautics; Flight
sufficiently to exert their pull on the spring scales without being
affected by the supply and exhaust of water.
[Illustration: PL. 82
DYNAMOMETER TESTS OF LARGE ENGINE]
[Illustration: PL. 83
DYNAMOMETER TESTS OF LARGE ENGINE]
[Illustration: PL. 84
DYNAMOMETER TESTS OF LARGE ENGINE]
The water for cooling the cylinders is led from the bottom of the
tank ‹E› to the circulating pump ‹F›, supported in a discarded lower
pyramid of the aerodrome frame, the pump being driven by the small
vertical shaft, as already described. The water, after passing
through the pump and the engine cylinders, is led back to the upper
part of the tank. By suitable connections to the water mains and
sewer, the water in the tank is kept at any desired temperature. The
gasoline supply tank is seen on the left-hand side of the testing
frame, as viewed in Plate 82, the carburetor being placed below it
and the gas supply pipe from the carburetor passing through the
gasoline tank. Instead of jacketing the carburetor, a grid formed
of thin copper tubes is supported just above the multitude of small
air pipes leading into the carburetor, and some of [p249] the
hot water from the engine is by-passed through this grid and thus
warms the air as it passes into the carburetor. The small pipe that
by-passes this water through the grid is seen connected to the outlet
water pipe just above the cylinders, a small butterfly valve in the
outlet pipe enabling the amount of heated water passing through
the grid to be controlled. The return from the grid is by means
of the small pipe leading to the top of the large water tank. The
tachometer, which gives instantaneous readings of the speed of the
engine, is seen at ‹G›, where it is at all times in full view of the
operator.
These dynamometers proved to be excellently suited for the testing
work, and far ahead of anything else the writer has ever found for
engine testing. Since the power required to rotate the rotor plates,
with a uniform amount of water in the drums, varies as the cube of
the speed, it is readily seen that it is impossible for the engine to
race or injure itself by running away, as frequently happens where
there is no engine governor and Prony brakes are used to measure the
power.
Public-domain text, read in full here on John Shaqi.
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