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
India rubber is the source of power to which the designer of a
working model naturally turns, where it is desirable that it shall
be, above all, light and free from the necessity of using complicated
mechanism. Rubber motors were, [p022] therefore, used on all of
the earlier models, and served as the basis of calculations made
to determine the amount of power that would be required to propel
aerodromes with other sources of energy.
Some of the disadvantages inherent in the use of rubber are at
once apparent, such as the limited time during which its action is
available, the small total amount of power, and the variability in
the amount of power put forth in a unit of time between the moment of
release and the exhaustion of the power. In addition, serious, though
less obvious difficulties, present themselves in practice.
There are two ways in which rubber can be used; one by twisting a
hank of strands, and, while one end is held fast, allowing the other
to revolve; the other, by a direct longitudinal stretching of the
rubber, one end being held fast and the other attached to the moving
parts of the mechanism. The former method was adopted by Pénaud,
and was also used in all of my early constructions, but while it is
most convenient and simple in its (theoretical) application, it has,
in addition to the above drawbacks, that of knotting or kinking,
when wound too many turns, in such a way as to cause friction on
any containing tube not made impracticably large, and also that of
unwinding so irregularly as to make the result of one experiment
useless for comparison with another.
In 1895, some experiments were made in which the latter method was
used, but this was found to involve an almost impracticable weight,
because of the frame (which must be strong enough to withstand the
end pull of the rubber) and the mechanism needed to convert the pull
into a movement of rotation.
As the power put forth in a unit of time varies, so there is a
corresponding variation according to the original tension to which
the rubber is subjected. Thus in some experiments made in 1889 with
a six-bladed propeller 18.8 inches in diameter, driven by a rubber
spring 1.3 inches wide, 0.12 inch thick and 3 feet long, doubled, and
weighing 0.38 pound, the following results were obtained:
Number of twists of rubber 50 75 100
Time required to run down 7 sec. 10 sec. 12 sec.
Foot-pounds developed 37.5 63.0 124.6
Foot-pounds developed per min. 321.4 378.0 623.0
Horse-power developed 0.0097 0.0115 0.0189
Thus we see that, with twice the number of turns, more than three
times the amount of work was done and almost twice the amount of
power developed, giving as a maximum for this particular instance 328
foot-pounds per pound of rubber.
Public-domain text, read in full here on John Shaqi.
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