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
With a gasoline engine, however, the conditions are very greatly
altered. Here the engine constitutes practically the entire weight
of the power plant, only such accessories as the ignition coil,
batteries, and carburetor being available for lowering the center of
gravity, unless the fuel, cooling water tanks and radiator be placed
below the engine and the liquids forced up by means of a pump. In
making the first designs for the large aerodrome, therefore, it was
found that it would be practically impossible to make the relative
positions of the center of gravity and line of thrust the same as had
existed in model No. 6, however desirable it might be. The center of
gravity could be brought appreciably lower than the line of thrust
only by placing the gasoline engine in a plane considerably below
that of the propellers, and this necessitated the addition of at
least two more sets of gears with heavy bearings and braces. Besides
this almost prohibitive factor of weight, it was also foreseen that
great difficulty would be experienced in keeping even the two sets
of bevel gears already necessary aligned and in proper condition for
efficiently transmitting the power to the propellers unless the frame
and other parts were made prohibitively heavy. It was, therefore,
found necessary to bring the center of gravity practically in the
same plane with the line of thrust, which made its general features
as regards equilibrium more nearly resemble those of model No. 5 than
of No. 6.
The weight of the aviator, it is true, constituted an appreciable
part of the flying weight of the large machine, and it at first
seemed possible to lower the center of gravity by placing him at a
considerable distance below the line of thrust. But it was recognized
from the beginning that the aviator would probably have to give a
great deal of attention to any form of engine in order to insure its
working properly, and his position must, therefore, be selected with
a view to the proper supervision of the engine and without regard to
its effect on the center of gravity.
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