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
plate and the head of the drum to provide room for the exhaust-valve
cam and its co-acting punch rods. The starboard bed plate is fastened
to the starboard head of the drum by bolts which draw the web of the
bed plate against the face of the drum. The sparking gears are driven
by means of a gear formed on a sleeve which telescopes over the hub
of the starboard drum, and has a bearing thereon, the end of the
sleeve terminating in a ring which is fastened to the crank shaft.
Since the five connecting rods must center on the one crank pin, the
bronze shoes in which they terminate can occupy only a portion of the
circumference of the pin, and with the relative proportions which
here existed between the length of stroke of crank and the length of
the connecting rod, the circumferential width of the connecting-rod
shoes was slightly less than sixty degrees, thus leaving uncovered
a crank space of about one-sixth of the circumference, which it was
necessary to have in order to provide room for the change in relative
position of the shoes due to the angularity of the connecting rods.
In [p238] the experimental engine the connecting-rod shoes were
all given their bearing directly on the crank pin, as heretofore
described, being held in contact therewith by means of cone nuts,
which were screw-threaded to the crank pin, the taper of the cones
permitting adjustment for wear. This method of connecting these
parts to the crank pin is the usual plan of connecting three or
more connecting rods to one crank pin. So much trouble had been
experienced with the water jackets and with minor defects in the
experimental engine that no long runs had been possible with it,
and consequently no trouble had been experienced because of the
small amount of bearing area provided by this method of joining the
connecting rods to the crank pin. When, however, the new engine
was completed it was found that after working at high power for a
few minutes the connecting-rod shoes heated so rapidly that it was
impossible to run the engine for more than ten or twelve minutes, the
excessive heating of the shoes causing a great diminution in power
besides the danger of serious damage if the tests were continued
longer. At first this defect seemed almost fatal, as there appeared
to be no way of providing sufficient bearing area for the five
connecting rods on one crank pin. Happily, however, the writer was
able to overcome this defect by an improved design which enables all
five connecting rods to operate on the one crank pin, and at the
same time provides each with the full amount of bearing area which
it would have were it the only connecting rod operating on the crank
pin. This arrangement consists essentially of a main connecting rod
formed of a steel forging terminating in a sleeve which encircles
the crank pin and is provided with a bronze lining for giving a
proper bearing surface between the connecting rod and the crank pin,
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