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The Electrical experimenter

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May, 1917<br />

ELECTRICITY<br />

is being rapidly introduced<br />

in tile new art of Aeronautics<br />

as the illustrations herewitli<br />

tend to testify. <strong>The</strong> greatest development<br />

in the art of flying is<br />

the aerial limousine or so-called .lulophmtillustrated<br />

in I'ig. 1, which was exhibited<br />

at the recent aeroplane show held in New<br />

^ork City. This aeroplane is built in the<br />

form of an automobile limousine<br />

and equipt with three<br />

planes for the sustaining surface.<br />

Aside from its perfect<br />

mechanical features its electrical<br />

e(|uipment is exceedingly<br />

interesting, as the engine is<br />

automatically started by means<br />

of an electric motor installed<br />

exactly the same as the mod-<br />

ern ntitnmoliilo engine electric starter. <strong>The</strong><br />

engine develops 1(X) horsepower and drives<br />

a foiir-bladed propeller place at the rear.<br />

<strong>The</strong> interior lighting is accomplisbt entirely<br />

by electric lamps and its ignition is of<br />

the very latest electrical design. .Mtho it<br />

may seem that the machine was not made<br />

for speed, yet it has a speed range of sixtyr<br />

five miles per hour and can si tain a weight<br />

of "10 pounds. Tt can carry two passengers<br />

and a pilot.<br />

<strong>The</strong> slntlcmomclcr illustrated in Fig. 2<br />

is an electric instrument devised to warn<br />

the aviator when his machine is approaching<br />

a stalling condition by indicating that<br />

THE ELECTRICAL EXPERIMENTER<br />

Electrifying the Aeroplane<br />

the minimum air speed has been reached.<br />

It is mounted in any convenient position<br />

where the air flow is unobstructed.<br />

<strong>The</strong> stallemometcr is adjustable for any<br />

desired air speed, depending on the aeroplane<br />

on which it is installed. When the<br />

predetermine! speed is reached, an electric<br />

contact is closed in the stallemometer, closing<br />

the circuit thru an indicating lamp<br />

miniiited on the instrument hoard stationed<br />

ill front of the pilot.<br />

.'\n incidence indicator increases the efficiency<br />

of an aeroplane by warning the aviator<br />

before he stalls and by enabling him to<br />

get the best. climbing and gliding angles out<br />

of his machine.<br />

<strong>The</strong> transmitter of the Incidence Indicator<br />

in Fig. ,1. is mounted on a forward strut<br />

so as not to interfere with anv part of the<br />

plane. <strong>The</strong> lamp bank or indicator is on<br />

the instrument cowl, always visible to the<br />

nilot observing other essential instruments.<br />

<strong>The</strong> red light warns the aviator before he<br />

stalls as well as when he begins climbing<br />

at a dangerous angle. <strong>The</strong> white lamp signals<br />

whenever the pilot dives at too steep<br />

an angle. <strong>The</strong> green light indicates the best<br />

climbing angle. I5eing of low voltage as<br />

well as low current consumption, the lights<br />

can be operated on a dry battery, encased<br />

in metal and installed wherever most convenient.<br />

<strong>The</strong> signals are regulated by a<br />

vane operated by the air stream.<br />

<strong>The</strong> lamp bank container is<br />

.seen in the background. Each<br />

lamp is equipt with the proper<br />

colored screen and each connected<br />

to the required contacts<br />

enclosed in the incidence indicator<br />

chamber. <strong>The</strong> lead wires<br />

are led thru one of the supporting<br />

tubes.<br />

.\viators wishing to know at<br />

anv lime tlie currect lore and all position<br />

of the machine, with reference to the<br />

horizontal, can read it on the scale of the<br />

dead-beat clinomeler illustrated at Fig. 4<br />

<strong>The</strong> operation of this instrument is simple.<br />

Whenever the clinometer is tipt forward<br />

or backward by the motion of the<br />

plane, this movement is re.gistered on a scale<br />

mounted on a wheel which is damped by<br />

floating in a liquid.<br />

If the aeronlane tips forward, the scale<br />

moves upward, indicating in degrees below<br />

the zero line the exact angle. If the machine<br />

tips backward, the scale moves down-<br />

(Continued »i f'a

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