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 sparking apparatus comprised, first, a primary sparker similar
to the simplest form of such devices which have since come into
common use, where a cam driven by the engine co-acts with a pawl
on the end of a spring, but in this case, as this sparker was used
for all five cylinders, the cam was driven at a speed of two and
one-half times that of the engine shaft, thus making and breaking the
primary circuit five times in each two revolutions of the engine.
Second, a spark coil, the primary terminals of which were connected
to the primary sparker and to a set of dry batteries. Third, a
secondary distributor consisting of a disc carrying a contact brush
and driven at a speed one-half that of the engine, this brush being
constantly connected through a contact ring to one of the terminals
of the high-tension side of the spark coil and running over the
face of a five-section commutator, each of the sections of which
was connected to a spark plug, the other high-tension terminal of
the spark coil being, of course, grounded on the engine frame. This
sparking apparatus was first constructed by using blocks of red
fibre for insulation. After the engine was completed and was being
tested difficulties were met with in the sparking apparatus which
at that time appeared inexplicable. After a great deal of annoyance
and loss of time it was finally discovered that the red fibre was
not as good an insulating medium as it was supposed to be, owing
to the zinc oxide used in making it. In damp weather the sparking
apparatus absolutely refused to work, and it was found that the
moisture in the air caused the zinc oxide in the fibre to nullify its
insulating qualities. This trouble, after being located, was cured by
substituting hard rubber for the red fibre.
At the time when this engine was built, as well as earlier when the
experimental engine was built, it was impossible to procure any wire
which had been properly insulated to withstand the high voltages
necessary for the connections between the high-tension side of the
spark coil and the secondary distributor, and from the secondary
distributor to the spark plugs in the cylinders. While at this time
this appears a very simple matter, yet the trouble experienced and
[p242] the delays caused by the lack of such small accessories
which are now so easily procurable were very exasperating, and it
was finally necessary to insulate these wires by covering them with
several thicknesses of ordinary rubber tube of different diameters
telescoped over each other.
In the early tests of this new engine, which were made with it
mounted on a special testing frame and delivering its power to the
water-absorption dynamometers, the engine was operated without any
fly wheels, and, so far as its smoothness of operation was concerned
and its ability to generate its maximum power, it did not require any.
Public-domain text, read in full here on John Shaqi.
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