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 aviator’s car was therefore designed to occupy the entire
available space between the engine and the front bearing points, and
between the two main tubes of the main frame, thus allowing him a
space of something like three feet by five feet. The car itself was
shaped like a flat-bottomed boat, the bottom being approximately
level with the bottom of the lower pyramid. It had a guard rail
of steel tubing eighteen inches above the floor, with a cloth
covering drawn over the frame to decrease the head resistance of the
appurtenances of the engine which were placed at the rear end of the
car. The car was supported by vertical wires passing from its bottom
up to the main frame, and was prevented from longitudinal or side
motion by being fastened at the front to the cross-rod connecting the
front bearing points, and at the rear to the lower pyramid. A light
wooden seat extended fore and aft of the car at a height of about two
feet from the floor, this seat resting on blocks of sponge rubber to
absorb some of the tremor which existed in the whole aerodrome when
the engine and propellers were working at high speed. The aviator
was thus free to stand, to sit sidewise or to straddle the seat,
and while the network of wires surrounding him prevented any great
possibility of his being thrown out, yet there was a comparatively
large opening between the guy-wires passing overhead which permitted
him to climb out of the machine.
In order to enable the aviator to know exactly how the engine was
operating, a tachometer, giving instantaneous readings of the number
of revolutions, was connected by a suitable gear to one of the
transmission shafts and placed where it could readily be seen.
During 1898 and 1899 considerable time and attention had been given
to designing an instrument to be carried by the aerodrome which would
automatically record the number of revolutions of the engine, the
velocity and direction [p186] of the wind relative to the machine,
the height of the aerodrome as shown by a specially sensitive aneroid
barometer, and the angle of the machine with the horizontal plane
of the earth. The construction of this instrument was undertaken by
a noted firm of instrument makers, but after many months of delay,
during which it was several times delivered as being complete,
only to be returned for further work, it was finally condemned as
unsatisfactory, and it was decided not to encumber the machine with
such a delicate apparatus, which, even if perfectly made, could not
be depended on to work properly when mounted on the aerodrome frame,
in which there was a constant, though minute, tremor due to the high
speed and power of the engine.
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