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
In carrying out these plans, however, of making the cylinders of
steel, numerous constructional difficulties were encountered which
could not be foreseen when the design was made. Had they been
foreseen, provision for obviating them could easily have been made.
As will be seen from the drawing, Plate 78, the engine cylinders
consisted primarily of a main outer shell of steel one-sixteenth
of an inch thick, near the bottom end of which was screwed and
brazed a suitable flange, by which it was bolted to the supporting
drum or crank chamber. These shells, which were seamless, with the
heads formed integral, were designed to be of sufficient strength
to withstand the force of the explosion in them, and, in order to
provide a suitable wearing surface for the piston, a cast-iron
liner one-sixteenth of an inch thick was carefully shrunk into
them. Entering the side of the cylinder near the top, was the
combustion chamber, machined out of a solid steel forging, which
also formed the port which entered the cylinder and was fastened to
it by brazing. The water jackets, which were formed of sheet steel
.020 inch thick, were also fastened to the cylinder by brazing,
and it was in connection with the brazing of these water jackets
that the first serious difficulty was met in the construction of
the engine. In the first place, as the jackets were of an irregular
shape and of a different thickness of metal from the walls of the
cylinder to which they were joined, the expansion and contraction
due to the extreme heat necessary for properly brazing the joints
caused such serious strains in various and unexpected directions
that it was only by exercising the very greatest care and patience
that a completely tight joint at all points of the jacket could be
secured. In the second place, the size of the cylinders and the
consequently large extent of water-jacket surface, complicated the
problem. The maintenance over this large surface of the extreme
heat necessary for brazing involved discomfort and, indeed, actual
suffering to the person engaged in the work, and much care and skill
were demanded in so distributing the heat that the temperature
of the surface of the jackets would be uniform enough to prevent
serious strains from expansion and contraction. As no workman could
be found either competent to do the work or willing to undergo the
personal discomfort, the writer was obliged to do all this brazing
work himself. Besides the difficulties due to the expansion and
contraction of the jackets while they were being brazed, the greatest
care had to be exercised to avoid heating the cylinders so hot as to
weaken the [p236] joint where the explosion chambers were joined to
the cylinders, which, of course, had been brazed before the jackets
were fitted to them preparatory to brazing them.
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