The Propeller

Very little effort has been made to utilize paddle wheels for aerial

propulsion; the screw is almost universally employed. Every one knows

that when a bolt turns in a stationary nut, it moves forward a distance

equal to the _pitch_ (lengthwise distance between two adjacent threads)

at every revolution. A screw propeller is a bolt partly cut away for

lightness, and the "nut" in which it works is water or air. It does

not move forward quite as much as its pitch, at each revolution,

because any fluid is more or less slippery as compared with a nut of

solid metal. The difference between the pitch and the actual forward

movement of the vessel at each revolution is called the "slip," or

"slip ratio." It is never less than ten or twelve per cent in marine

work, and with aerial screws is much greater. Within certain limits,

the less the slip, the greater the efficiency of the propeller. Small

screws have relatively greater slips and less efficiency, but are

lighter. The maximum efficiency of a screw propeller in water is under

80%. According to Langley's experiments, the usual efficiency in air

is only about 50%. This means that only half the power of the motor

will be actually available for producing forward movement--a conclusion

already foreshadowed.

In common practice, the pitch of aerial screws is not far from equal

to the diameter. The rate of forward movement, if there were no slip,

would be proportional to the pitch and the number of revolutions per

minute. If the latter be increased, the former may be decreased.

Screws direct-connected to the motors and running at high speeds will

therefore be of smaller pitch and diameter than those run at reduced

speed by gearing, as in the machine illustrated on page 134. The number

of blades is usually two, although this gives less perfect balance than

would a larger number. The propeller is in many monoplanes placed in

_front_: this interferes, unfortunately, with the air currents against

the supporting surfaces.

There is always some loss of power in the bearings and

power-transmitting devices between the motor and propeller. This may

decrease the power usefully exerted even to _less_ than half that

developed by the motor.

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