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
Extending front and back from the hull were the tubes for supporting
the wings and tail, each one metre in length. The cross-framing for
carrying the propeller shafts was built of tubing 1.5 cm. diameter,
and the shafts themselves were of the same size. The ribs of the hull
were rings made of angle-irons measuring 1.50×1.75 cm., which were
held in place longitudinally by five 0.7 cm. channel bars.
As it had been learned in the preliminary experiments with the model
“beehive” boiler that the heated water would not of itself cause a
sufficiently rapid circulation to be maintained through the tubes to
prevent them from becoming red-hot, two circulating pumps were added
for forcing the water through the coils of the two forward and two
rear boilers respectively, the water being taken from the lower side
of the drum and delivered into the bottom of the coils, which were
united at that point for the purpose. A worm was placed upon each of
the propeller shafts, just back of the engines, meshing in with a
gear on a crank-shaft from which the pumps were driven. This shaft
rotated at the rate of 1 to 24, so that for 1200 revolutions of the
engine, it would make but 50, driving a single-acting plunger 1.2 cm.
in diameter and 2 cm. stroke.
Apparently all was going well until I began to try the apparatus.
First, there was a difficulty with the burner, which could not be
made to give forth the relative amount of heat that had been obtained
from the smaller model, and steam could not be maintained. With one
“beehive” connected with the compound engine, and a 70 cm. propeller
on the shaft, there were about 250 turns per minute for a space
of about 50 seconds, in which time the steam would fall from 90
pounds to 25 pounds, and the engine would stop. Then, as we had no
air-chamber on the pumps at the time, they would not drive the water
through the coils. Subsequent experiments, however, showed that the
boilers could be [p037] depended upon to supply the steam that the
compound engines would require; but after the whole was completed,
the weight, if nothing else, was prohibitory.
I had gone on from one thing to another, adding a little here and a
little there, strengthening this part and that, until when the hull
was finally completed with the engines and boilers in place, ready
for the application of the wings, the weight of the whole was found
(allowing 7 pounds for the weight of the wings and tail) to be almost
exactly 45 pounds, and nearly 52 pounds with fuel and water. To this
excessive weight would have to be added that of the propellers, and
as the wings would necessarily have to be made very large in order to
carry the machine, and as the difficulties of launching had still to
be met, nothing was attempted in the way of field trials, and with
great disappointment the decision was made in May, 1892 (wisely, as
it subsequently appeared) to proceed no further with this special
apparatus.
Public-domain text, read in full here on John Shaqi.
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