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
The first set of pistons for this engine were similar in design to
those shown in the assembled drawings, except that they had side
walls and heads which were twice as thick as those shown. These
lighter pistons were constructed later, and were just as good as
the earlier and heavier ones. It will be noted that the pistons
have two deep but thin ribs reinforcing the head. The pistons were
slightly tapered from the middle, where they were .005 inch smaller
than the cylinder bore, toward the outer end, where they were .0075
inch smaller [p240] than the bore. The outer piston ring was .0035
inch narrower than its groove, the second one .003 inch, the third
.0025 inch, and the inner one .002 inch narrower than its groove.
The rings were bored one-sixteenth inch off center with the exterior
surface, and had one-eighth inch diameter of spring. They were of
the lap-joint type, with the sides of the laps carefully fitted and
only one-sixty-fourth-inch clearance at the ends of the laps to allow
for thermal expansion. As no grinding facilities were obtainable in
Washington, the cylinders were carefully bored smooth and free from
taper, and the pistons were worn in to a perfect fit by running them
in by a belt for twenty-four hours, with copious oil supply.
The main connecting rod was 7/8-inch diameter and solid, while
the other four were of the same diameter but with a 5/8-inch hole
in them. The gudgeon pins in the pistons were hollow steel tubes
7/8-inch diameter and case-hardened, and were oiled entirely by the
oil thrown off by centrifugal force from the crank-pin bearing, the
oil running along the connecting rods and through suitable holes at
the heads into oil grooves in the bronze bushings in these heads.
Public-domain text, read in full here on John Shaqi.
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