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
The steering and control in the air are arranged in principle exactly
as in a small aeroplane, but it was not an easy problem to arrange that
this 14-ton boat could be handled by one man of only normal strength.
To insure easy operation, each control surface was carefully balanced
in accordance with experiments made in a wind-tunnel on a model of
it. The operating cables were run through ball-bearing pulleys, and
all avoidable friction eliminated. Finally, the entire craft was
so balanced that the centre of gravity of all weights came at the
resultant centre of lift of all lifting surfaces, and the tail surfaces
so adjusted that the machine would be inherently stable in flight. As
a result, the boat will fly herself and will continue on her course
without the constant attention of the pilot. However, if he wishes to
change course, a slight pressure of his controls is enough to swing the
boat promptly. There is provision, however, for an assistant to the
pilot to relieve him in rough air if he becomes fatigued, or wishes to
leave his post to move about the boat.
In the design of the metal fittings to reduce the amount of metal
needed a special alloy steel of 150,000 pounds per square inch tensile
strength was used. To increase bearing areas, bolts and pins are made
of large diameter but hollow.
A feature that is new in this boat is the use of welded aluminum tanks
for gasoline. There are nine 200-gallon tanks made of sheet aluminum
with welded seams. Each tank weighs but 70 pounds, or .35 pounds per
gallon of contents, about one-half the weight of the usual sheet-steel
or copper tank.
Loaded, the machine weighs 28,000 pounds, and when empty, but including
radiator, water, and fixed instruments and equipment, 15,874 pounds.
The useful load available for crew, supplies, and fuel is, therefore,
12,126 pounds. This useful load may be put into fuel, freight, etc.,
in any proportion desired. For an endurance flight there would be a
crew of 5 men (850 pounds), radio and radiotelephone (220 pounds), food
and water, signal-lights, spare parts, and miscellaneous equipment (524
pounds), oil (750 pounds), gasoline, 9,650 pounds. This should suffice
for a flight of 1,400 sea miles. The radio outfit is of sufficient
power to communicate with ships 200 miles away. The radiotelephone
would be used to talk to other planes in the formation or within 25
miles.
The principal dimensions and characteristics of the NC type may be
summarized as follows:
Engines 4 Liberty
Power 1,600
Wing span 126 upper—94 feet lower
Length 68 feet 5½ inches
Height 24 feet 5⅛ inches
Weight, empty 15,874 lbs.
Weight, loaded 28,000 lbs.
Useful load 12,126 lbs.
Gravity-tank 91 gals. capacity
Fuel-tanks 1,800 gals. capacity
Oil-tanks 160 gals. capacity
FIRST AERIAL STOWAWAY
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