Aircraft : $b its development in war and peace and its commercial futureDavid, Evan John
History
Aircraft : $b its development in war and peace and its commercial future
David, Evan John
Aeronautics; Airplanes
In laying down this motor we have without reserve selected the best
possible practice from both Europe and America. Practically all
features of this motor have been absolutely proved out in America by
experimental work and manufacturing experience in the Hall-Scott and
Packard plants, and we are, therefore, willing to unhesitatingly stake
our reputations on this design, providing we are allowed to see that
our design and specifications are absolutely followed.
The motor is to be of the eight-cylinder type, with cylinders set at
an included angle of 45 degrees. The cylinders are of the individual
type, made out of steel forgings with jackets welded on. The bore is
five inches and the stroke seven inches, giving a piston displacement
of 1,100 cubic inches. The crank-shaft is of the five-bearing type
with all main bearings 2⅜ inches in diameter, and all crank-pin
bearings 2¼ inches in diameter. The connecting-rods are of the
I-beam straddle type. This motor is of the direct-driven type with a
maximum speed of 1,700 r. p. m. This motor will have a maximum output
of 275 horse-power at 1,700 r. p. m. It will weigh 525 to 550 pounds,
but we feel very sure of the lower figure. It will have a gasoline
economy of .50 pounds of fuel per horse-power hour or better; it will
have an oil economy of .04 pounds of oil per horse-power hour or
better. Complete with water and radiator, this motor will not weigh
more than 675 pounds, if a properly constructed radiator is used and
placed high above the motor.
To obtain the above-mentioned weights it will be necessary to use the
fixed type of propeller hub which has been thoroughly proved out by
Hall-Scott practice. In order to obtain the above-mentioned weights
it will also be necessary, as mentioned above, to use the very best
material, workmanship, and heat treatment.
Complete detail and assembly drawings, as well as parts list and
material specifications, can be completed at the Packard factory under
our direction in less than four weeks. We believe that a sample motor
can also be completed in approximately six weeks if money is used
without stint. As soon as the drawings, specifications, and sample
motor have been finished, complete information would, of course, be
available so that any high-grade manufacturer could either make parts
for this motor or manufacture it complete.
In laying down this design we have had in mind the extreme importance
of interchangeability, as a well-laid, comprehensive programme
which has for its base interchangeability of important parts,
such as cylinders, will speed output and reduce ultimate cost to
an astonishing extent. Europe is suffering right now from lack of
uniformity of design, but it is too late for them to change their
plan. We, however, can take a leaf out of their book and start right.
Public-domain text, read in full here on John Shaqi.
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