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
“Unfortunately there is a limit set to this process of increasing
the steam supply, quite aside from conditions inherent in the
method. This is due to the fact that a certain speed of efflux
cannot be exceeded without putting the flame out. Suppose, for
instance, in Fig. 12, that a gas generated from a liquid is ignited
at the end of the Bunsen burner ‹F›; then if the velocity of efflux
of mixed gas and air in the direction ‹AB› from the mouth of ‹F›
exceeds the velocity of combustion in the direction ‹BA›, the flame
will obviously be carried away from the mouth of the tube and
dissipated. This state of things is actually realized at pressures
exceeding about 15 lbs., depending on the degree of mixture of
the combustible gases used, and therefore on apparently haphazard
conditions connected with the jet, the air holes, the air supply,
etc.
[Illustration: FIG. 12.]
[Illustration: FIG. 13.]
“If, however, the velocity of the jet at the point of efflux be
checked by an obstruction like a cylinder ‹C›, Fig. 13, placed
co-axially with the burner tube ‹F›, the speed of combustion will no
longer be exceeded (supposing ‹C› properly chosen) and flames will
then burn from high-pressure gas. In this way flames were maintained
generated from alcohol gas at even 40 lbs. and above.
[Illustration: FIG. 14.]
“The gas escaping from the Bunsen burner is never sufficiently
aërated to burn completely. Otherwise there would (in general) be
explosions in the tube ‹F›. A part of this air is supplied at the
mouth of the boiler ‹B›, Fig. 14, and the amount available here will
depend on the velocity of the jet ‹F›. Hence it does not follow
that a high-pressure burner like that in Fig. 11 will supply a
proportionate amount of heat, since its jet suction is not intense
and the combustion within the boiler is incomplete. This difficulty
may be remedied by placing [p074] air holes in the jacket of the
boiler, provided the boiler be wrapped loosely enough not to chill
the flame below ignition. It is with reference to this effect that
the boilers, Fig. 11, were wound. A number of rifts ‹aaa›, Fig. 15,
are then left in the jacket through which air may enter in virtue of
the burner flame acting as a jet at the mouth of the boiler.
“When so constructed the flame at first enters the inner coil only;
but after a little while it suddenly spreads out throughout the
whole interior space and envelops the coils. This sudden expansion
is due, probably, to the assumption of the spheroidal state by the
water within the coils, the current now flaring on an enveloping
cushion of steam. The pump must work well, for deficient water means
a hot tube and deficient steam, or eventually a rupture of the tube.
Public-domain text, read in full here on John Shaqi.
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