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
lattice flooring over pontoons, moored at the rear end of the boat,
as clearly seen in Plate 38. In order to raise the aerodrome frame
from the raft to the upper works, a large, but light, mast and boom,
with suitable stays were provided. As the wings, when mounted in
their proper position on the aerodrome, would be interfered with by
such a mast, the mast and boom were so devised as to be capable of
rapid erection and dismounting, only five minutes being necessary for
either operation. In Plate 38 the mast and boom are seen in position
in Fig. 3, while in Figs. 1 and 2 they have been dismounted.
The construction of the launching track and car was begun in
November, 1899, but their completion was long delayed, as they were
frequently put aside for the more immediately important parts of
the work. Moreover, the arrangement of the struts and clutch of
the launching car depended entirely on the form and dimensions of
the frame of the aerodrome, which could not be entirely decided
until a proper engine had been secured and tested in the frame to
determine what modifications of it were necessary. In the spring of
1902, however, the launching car was entirely finished and a number
of tests of the large engine were made in the shop with the frame
mounted in position on the car.
From the description of the “overhead” launching apparatus (Part
I, Chapter X) which had proved so successful in the tests of the
models, both in 1896 and in the later experiments of 1899, it will be
recalled that the essential features of it were a track and a light
car with three hinged struts which extended below the body of the
car, and against which suitable co-acting bearing points attached to
the frame of the aerodrome were tightly drawn by means of a clutch
which gripped a special fitting fastened to the aerodrome frame near
the central point of its length. After the engine of the aerodrome
had been started and got to running at full speed, the car was
released and moved forward along its track by the combined force of
the thrust of the propellers and the pull of the coiled launching
springs. Just before the car reached the forward end of the track, a
cam at this point caused the clutch to open and release [p158] the
aerodrome, which immediately dropped slightly, as it had purposely
not quite reached a speed sufficient to cause it to soar. This slight
drop of the aerodrome, even if it were only a fraction of an inch,
made it possible for the hinged struts, against which it had been
held by the clutch, to be folded up by their special springs against
the floor of the car, thus leaving the aerodrome free in the air
without danger of entanglement.
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