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
Suitable flanges and collars were brazed to the propeller shafts;
but, for convenience in assembling, the flanges by which the main
transmission shafts were connected to the crank shaft of the engine
were at first fastened to the shafts by screw-threads, the threads
being in the proper direction to cause the flanges to jam against
the shoulders of the shafts when the engine turned in its normal
direction. This method of fastening, however, caused serious trouble,
owing to the flanges jamming so tight that it became impossible to
unscrew them after they had once been used in driving the propellers.
The usual provisions of keys and key-ways adopted in general
engineering practice, where solid shafts are employed, were, of
course, out of the question, since the shaft would have to be greatly
increased in thickness throughout its entire length [p177] merely
to provide the extra metal at the small place in which the key-ways
were formed. Taper pins either sheared off or very soon stretched
the holes so badly as to leave the parts loose, and were otherwise
very unsatisfactory. The method finally adopted, which proved very
successful, was that of forming integral with the couplings shallow
internal tongues and grooves which fitted corresponding tongues and
grooves either in the exterior surface of the shafts or in collars
brazed to them at the proper point. The form of flange coupling, in
which bolts draw the two flanges tightly together, was also a source
of considerable trouble and delay, which was finally overcome by
forming shallow tongues and grooves in the faces of the flanges, the
tongues taking up the torsion and relieving the bolts which held the
flanges together of all strain except one of slight tension. The same
difficulties experienced in mounting the couplings on the shafts were
met with in connection with the gears, both on the propeller and
transmission shafts, and were finally obviated in a manner similar to
that described above.
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