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
These engines, driven either by steam or by carbonic-acid gas
developed 0.035 horse-power at the Prony brake, giving 750
revolutions of the 45 cm. propellers, and lifting about 1/5 of the
total weight which it was necessary to provide for in actual flight.
A higher rate of revolution and a better lift were occasionally
obtained, but there was little more hope with this than with the
preceding models of obtaining power enough to support the actual
weight in flight, although such sacrifices had been made for
lightness that every portion of the little model had been reduced to
what seemed the limit of possible frailty consistent with anything
like safety. Thus the midrod was lighter than that of No. 1, being
only 1 cm. in outside diameter. The frame was made of thin wooden
strips 5 mm.×3.5 mm., united by light steel rings. The cross framing
carrying the engines was also of wood, and was formed of four strips,
each 7 mm.×3 mm. The shafts were but 4 mm. in diameter.
As these engines did not give results that were satisfactory, when
using carbonic-acid gas, experiments were commenced to secure a
boiler that would furnish the requisite steam. As the “beehive”
boiler had proved to be too heavy, and as the steam obtained from it
had been inadequate to the requirements, something else had to be
devised. A few of the boilers used in 1892 are shown in Fig. 3. The
one marked ‹A› is one of the “beehives,” while an element of another
form tried is that marked ‹B›. It consisted of 3/8-inch copper tubes
joined to a drum of 10-oz. copper. This was made in May, 1892, and
was tested to a pressure of 50 atmospheres, when it burst without any
tearing of the metal.
In July another boiler like that shown at ‹C› in Fig. 3 was made.
This was formed of tubes 3 cm. in diameter, and weighed 348 grammes.
It carried about 300 grammes of water and stood a steam pressure of
125 pounds per square inch, but failed to maintain sufficient steam
pressure.
Accordingly, in the same month, a third boiler like that shown at
‹D› was built. It consisted of a tube 12 inches long to which were
attached fifteen 1/4-inch tubes each 7 inches long, in the manner
shown. The heating surface of this boiler, including the tubes and
the lower half of the drum, amounted to 750 square cm., and it was
thought that this would be sufficient to supply steam for a flight of
a [p040] minute and a half. But when a test was made, it also was
found to be deficient in steaming power even after changes were made
in it which occupied much time.
By the first of October, 1892, there had been built one large
aerodrome that could not possibly fly, a smaller one, No. 1, on 2/5
the linear scale of No. 0, with a pair of engines but no means of
driving them, and the still smaller No. 2 with a boiler that was yet
untried.
Public-domain text, read in full here on John Shaqi.
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