Flying Machines TodayEnnis, William D. (William Duane)
History
Flying Machines Today
Ennis, William D. (William Duane)
Aeronautics; Flying-machines
The mechanism of an orthopter would be relatively complex, and the
flapping wings would have to "feather" on their return stroke. The
flapping speed would have to be very high or the surface area very
great. This last requirement would lead to structural difficulties.
Propulsion would not be uniform, unless additional complications were
introduced. The machine would be the most difficult of any type to
balance. The motion of a bird's wing is extremely complicated in its
details--one that it would be as difficult to imitate in a mechanical
device as it would be for us to obtain the structural strength of an
eagle's wing in fabric and metal, with anything like the same extent of
surface and limit of weight. According to Pettigrew, the efficiency of
bird and insect flight depends largely upon the elasticity of the wing.
Chatley gives the ratio of area to weight as varying from fifty (gnat)
to one-half (Australian crane) square feet per pound. The usual ratio
in aeroplanes is from one-third to one-half.
About the only advantages perceptible with the orthopter type of
machine would be, first, the ability "to start from rest without
a preliminary surface glide"; and second, more independence of
irregularity in air currents, since the propulsive force is exerted
over a greater extent than is that of a screw propeller.
The Helicopter
The _gyroplane_ or _helicopter_ was the type of flying machine
regarded by Lord Kelvin as alone likely to survive. It lifts itself
by screw propellers acting vertically. This form was suggested in
1852. When only a single screw was used, the whole machine rotated
about its vertical axis. It was attempted to offset this by the use
of vertical fin-planes: but these led to instability in the presence
of irregular air currents. One early form had two oppositely-pitched
screws driven by a complete steam engine and boiler plant. One of the
Cornu helicopters had adjustable inclined planes under the two large
vertically propelling screws. The air which slipped past the screws
imposed a pressure on the inclined planes which was utilized to produce
horizontal movement in any desired direction--if the wind was not too
adverse. A gasoline engine was carried in a sort of well between the
screws.
[Illustration: BRÉGUET GYROPLANE DURING CONSTRUCTION
(Helicopter type)]
The helicopter may be regarded as the limiting type of aeroplane, the
sail area being reduced nearly to zero; the wings becoming mere fins,
the smaller the better. It therefore requires maximum motor power and
is particularly dependent upon the development of an excessively light
motor. It is launched and descends under perfect control, without
regard to horizontal velocity. It has very little exposed surface and
is therefore both easy to steer and independent of wind conditions. By
properly arranging the screws it can be amply balanced: but it must
have a particularly stout and strong frame.
Public-domain text, read in full here on John Shaqi.
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