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 usual practice in balancing the rotating parts of an engine is to
attach [p247] balance weights to the crank arms which are prolonged
beyond the center of the crank shaft and on the opposite side from
the crank pin; the radius of rotation of these balance weights being
made approximately equal to the radius of the crank pin. But aside
from the constructional difficulties which would be introduced, it
was seen that if this plan was followed in this engine it would
require a very large additional weight. Since the amount of this
weight could be diminished in exact proportion to the increase of the
radius of rotation of the balance weights, it was at first decided
to attach the weights to the rims of the fly wheels, the relative
amount of weight attached to each wheel being inversely proportional
to its actual longitudinal distance from the crank-pin center. It
was very soon found that the attachment of these balance weights to
the fly wheel caused excessive strains on the rims of the wheels,
thereby causing them to go out of line. In order, therefore, to keep
the amount of balance weight small by carrying it at a considerable
distance from the center of the shaft, the weights were finally
arranged as clearly shown in the drawings, Plates 78 to 80. There
it is seen that the main portion of each of the balance weights
consists of a flat arm bolted between the flanges which couple the
transmission shafts to the engine shafts. The flat arm terminates in
a lozenge-shaped lug, additional weight being provided by a plate
fastened to one end of a tube, the other end of which terminates in a
collar fastened around the transmission shaft. The tube is inclined
at an angle of about thirty degrees with the flat balance arm, thus
acting as a brace to prevent the balance arm from wobbling, the plate
on the bracing tube being fastened to the lozenge-shaped lug by means
of small bolts.
The tabulated statement of the weight of this large engine is given
below. From this it will be readily seen that the net weight of
the engine proper is 124.17 pounds. The fly wheels were in no way
necessary to the engine itself, but were used solely for the purpose
of smoothing out the torque of the engine so that the transmission
shafts and propeller shafts might be kept down to the very minimum in
weight. Including the two fly wheels, the weight is 140 pounds.
Including the 20 pounds of cooling water the total weight of the
power plant is 207.47 pounds. Without flywheels the total weight is
191.64 pounds.
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