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
On account of these troubles with the water jackets and the cylinders,
it was decided to build some extra cylinders, not only because past
experience had suggested improvements in detail in the construction of
the jackets, which would prevent to a large extent the great troubles
which had been met with in the brazed joints, but also to insure
having sufficient cylinders to enable the engine to be always in
working condition, even though several of the cylinders might be out of
commission from slight imperfections in the jackets or at other points.
While the construction of these new cylinders involved a repetition
of the arduous task of brazing, yet the minor improvements which
were introduced [p237] proved eminently successful in providing
against future troubles from leaky jackets.
[Illustration: PL. 78
ENGINE OF AERODROME A. SECTION THROUGH CYLINDER AND DRUM]
[Illustration: PL. 79
ENGINE OF AERODROME A. END ELEVATION, PORT SIDE]
[Illustration: PL. 80
ENGINE OF AERODROME A. TOP PLAN]
[Illustration: PL. 81
ENGINE OF AERODROME A. ELEVATION STARBOARD BED PLATE, SPARKING
MECHANISM]
The general form of construction of the engine with the improved
cylinders will be readily understood from the drawings, Plates 78–81,
in which Plate 78 is a detail sectional view, previously referred to,
through one of the cylinders; Plate 79 is an end elevation of the
port side, Plate 80 is a plan view, and Plate 81 is an elevation of
the starboard bed plate which supports that side of the engine, and
by which it was fastened to the aerodrome frame, this view showing
particularly the sparking apparatus which was mounted on the bed
plate. The engine consists primarily of a single crank shaft provided
with a single crank pin, the shaft having bearings in a drum which
consists essentially of two heads. Arranged around the crank shaft
and attached at equidistant points of the drum are five cylinders.
Mounted on the port side of the crank shaft and close to the crank
arm is a small gear, which through suitable gears mounted on the port
head of the drum drives a double-pointed cam which has a bearing on
the exterior of the hub of the drum. The ratio of these gears is such
that the cam is driven at one-quarter the speed of the crank shaft,
and in the reverse direction. Mounted on the exterior side of the
port head of the drum are five punch rods, the upper ends of which
are within a sixty-fourth of an inch of being in contact with the
exhaust-valve stems of the cylinders, and on the lower end of these
rods are hardened-steel rollers which rest on the double-pointed
cam--this one cam thus serving to operate the exhaust valves of all
five of the cylinders. The port head of the drum is connected to
the port bed plate, by which it is supported, by means of a flanged
bushing in which are formed tongues and grooves which fit into
corresponding grooves and tongues formed in the hub of the drum, it
being necessary to have a certain amount of space between this bed
Public-domain text, read in full here on John Shaqi.
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