Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911 — John Shaqi
Langley Memoir on Mechanical Flight, Parts I and II: Smithsonian Contributions to Knowledge, Volume 27 Number 3, Publication 1948, 1911Langley, S. P. (Samuel Pierpont)
History
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
The first engines were of the oscillating type, with the piston-rod
connected directly to the crank; were very light, and were unprovided
with many of the usual fittings belonging to a steam engine, such as
rod or piston packing; and their construction was crude in comparison
with their successors. They were tested with the Prony brake and
found to be deficient in power, for with a steam pressure of 80
pounds to the square inch, they ran at the rate of 1170 revolutions
per minute, and developed only .363 horse-power. It soon became
evident that they were too light for the work that it was intended
that they should do, and steps were taken, even before the completion
of these tests, for the construction of a pair of more powerful
cylinders, which should also be provided with a special boiler for
the generation of the steam. Acting upon the supposition, in a saving
of steam, it was decided to work with compounded cylinders. As two
propellers were to be used, they were each fitted with a distinct
pair of cylinders working directly upon the shaft, but so connected
by gearing that they were compelled to turn at the same rate of speed.
The cylinders were of the inverted oscillating type, like the first
pair of engines, but, unlike them, they were single-acting. The
dimensions were: diameter of high-pressure cylinder 1.25 inches; low
pressure, 1.94 inches, with a common stroke of 2 inches, and with
cranks set opposite to each other so that one cylinder was always at
work. The cylinders were held at their upper ends by a strap passing
around a hollow conical trunk, which served the double purpose of
a support for the cylinders and an intermediate receiver between
them. This receiver had a mean inside diameter of 1.25 inches, with
a length of 4.75 inches, so that it had about twice the cubical
capacity of the high-pressure cylinder, while the displacement of
the low-pressure cylinder was about 2.5 times that of the high;
ratios that would have given satisfactory results, perhaps, had
the steam pressure and other conditions been favorable to the use
of the compound principle in this place. There were no valves for
the admission of the steam, for, inasmuch as the engines were
single-acting, it was possible to make ports in the cylinder-head
act as the admission and exhaust ports as the cylinder oscillated,
and thus avoid the complication and weight of eccentric and valves.
[p034]
These cylinders were set in a light frame at an angle of 25° with
each other, or 12.5° with the median line of the aerodrome, and drove
the long propeller shafts as shown in Plate 10, No. 0. At the extreme
forward end of the crank-shafts there was a pair of intermeshing
bevel gears which served to maintain the rate of revolution of the
two propellers the same.
[Illustration: FIG. 3. Boilers in use in 1891–1892.]
Public-domain text, read in full here on John Shaqi.
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