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 bevel gears originally constructed for transmitting the power
from the transmission shafts to the propeller shafts, were made of
case-hardened steel and were eight-pitch, twenty-five teeth, with
three-quarter inch width of face. The gears were very accurately
planed to give as perfect a form of tooth as possible, in order to
avoid loss of power in transmission, and although the manufacturer
who cut the teeth on them asserted at the time they were made
that they would not be capable of transmitting more than five
horse-power, yet they actually did transmit considerably more than
twelve horse-power on each set; but they were not strong enough
to transmit the full power of the large engine which was finally
used. The gears that were finally used were similarly constructed
of mild steel which was case hardened 1/64 of an inch deep after
they were finished, there being thirty-one teeth in the gear on the
transmission shaft and forty teeth in the one on the propeller shaft,
the teeth being eight-pitch, three-quarters of an inch face. These
light gears proved amply strong, and several times stood the strain
which they accidentally received when one of the propellers broke
while the engine was under full power, and thus threw the entire
fifty horse-power over on the other propeller, which was consequently
driven at a greatly increased speed.
Plain bronze bearings had been used throughout on the model
aerodromes, but in the construction of the large aerodrome
ball-bearings were used on all of the propeller and transmission
shafts, not only on account of the decreased loss through friction,
but also because ball-bearings can be built much lighter than solid
bronze ones, and, furthermore, do not present such great difficulties
in lubrication. However, owing to the limited size which it was
possible to secure for these bearings, because of their having been
originally designed for only twenty-four horse-power, and without any
margin for a later increase of the [p178] space in which they had
to be applied, they were never really large enough for the work they
had to do when transmitting the full power of the large engine. They
gave continual trouble, and were the source of delay which, while it
cannot be accurately measured, since there were often other causes,
yet might be conservatively estimated at not less than three or four
months. Such a delay, when reckoned in retrospect, can easily be seen
to have caused an expense which would have sufficed for almost any
change in the bearings, bed plates, etc., had the change been made
immediately after the bearings were found to give trouble. With the
better steel which it is now possible to obtain for the races of the
bearings, and with the high-grade balls now obtainable, the bearings
could be readily replaced without changing any other parts and still
be amply strong for the work.
PROPELLERS
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