aeroplanes-第20章
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the aeroplane。
If the power is transferred from the cylinder
to the engine shaft where it could deliver its output
without the use of a propeller; it would not
be so important to consider the matter of vibration;
but the propeller; if permitted to vibrate;
or dance about; absorbs a vast amount of energy;
while at the same time cutting down its effective
pull。
Aside from this it is dangerous to permit the
slightest displacement while the engine is running。
Any looseness is sure to grow worse; instead
of better; and many accidents have been
registered by bolts which have come loose from
excessive vibration。 It is well; therefore; to have
each individual nut secured; or properly locked;
which is a matter easily done; and when so secured
there is but little trouble in going over the machine
to notice just how much more the nut must
be taken up to again make it secure。
THE GASOLINE TANK。What horrid details have
been told of the pilots who have been burned to
death with the escaping gasoline after an accident;
before help arrived。 There is no excuse for
such dangers。 Most of such accidents were due
to the old practice of making the tanks of exceedingly
light or thin material; so that the least
undue jar would tear a hole at the fastening
points; and thus permit the gasoline to escape。
A thick copper tank is by far the safest; as this
metal will not readily rupture by the wrench which
is likely in landing。
WHERE TO LOCATE THE TANK。There has been
considerable discussion as to the proper place to
locate the tank。 Those who advocate its placement
overhead argue that in case of an accident
the aeroplane is likely to overturn; and the tank
will; therefore; be below the pilot。 Those who
believe it should be placed below; claim that in
case of overturning it is safer to have the tank
afire above than below。
DANGER TO THE PILOT。The great danger to the
pilot; in all cases of accidents; lies in the
overturning of the machine。 Many have had accidents
where the machine landed right side up; even
where the fall was from a great height; and the
only damage to the aviator was bruises。 Few; if
any; pilots have escaped where the machine has
overturned。
It is far better; in case the tank is light; to have
it detached from its position; when the ship strikes
the earth; because in doing so; it will not be so
likely to burn the imprisoned aviator。
In all cases the tank should be kept as far away
from the engine as possible。 There is no reason
why it cannot be placed toward the tail end of
the machine; a place of safety for two reasons:
First; it is out of the reach of any possible
danger from fire; and; second; the accidents in the
past show that the tail frame is the least likely to
be injured。
In looking over the illustrations taken from the
accidents; notice how few of the tails are even
disarranged; and in many of them; while the entire
fore body and planes were crushed to atoms;
the tail still remained as a relic; to show its
comparative freedom from the accident。
In all monoplanes the tail really forms part of
the supporting surface of the machine; and the
adding of the weight of the gasoline would be
placing but little additional duty on the tail; and
it could be readily provided for by a larger tail
surface; if required。
THE CLOSED…IN BODY。The closed…in body is a
vast improvement; which has had the effect of
giving greater security to the pilot; but even this
is useless in case of overturning。
STARTING THE MACHINE。The direction in which
improvements have been slow is in the starting
of the machine。 The power is usually so mounted
that the pilot has no control over the starting;
as he is not in a position to crank it。
The propeller being mounted directly on the
shaft; without the intervention of a clutch; makes
it necessary; while on the ground; for the propeller
to be started by some one outside; while
others hold the machine until it attains the proper
speed。
This could be readily remedied by using a
clutch; but in the past this has been regarded as
one of the weight luxuries that all have been trying
to avoid。 Self starters are readily provided;
and this with the provision that the propeller can
be thrown in or out at will; would be a vast improvement
in all machines。
PROPELLERS WITH VARYING PITCH。It is growing
more apparent each day; that a new type of
propeller must be devised which will enable the
pilot to change the pitch; as the speed increases;
and to give a greater pitch; when alighting; so
as to make the power output conform to the conditions。
Such propellers; while they may be dangerous;
and much heavier than the rigid type; will; no
doubt; appear in time; and the real improvement
would be in the direction of having the blades
capable of automatic adjustment; dependent on
the wind pressure; or the turning speed; and thus
not impose this additional duty on the pilot。
CHAPTER XI
FLYING MACHINE ACCESSORIES
THE ANEMOMETER。It requires an expert to
judge the force or the speed of a wind; and even
they will go astray in their calculations。 It is
an easy matter to make a little apparatus which
will accurately indicate the speed。 A device of
this kind is called an Anemometer。
Two other instruments have grown out of this;
one to indicate the pressure; and the other the
direction of the moving air current。
THE ANEMOGRAPH。While these instruments indicate;
they are also made so they will record the
speed; the pressure and the direction; and the device
for recording the speed and pressure is called
a Anemograph。
All these instruments may be attached to the
same case; and thus make a handy little device;
which will give all the information at a glance。
THE ANEMOMETROGRAPH。This device for recording;
as well as indicating the speed; pressure
and direction; is called an Anemometrograph;
The two important parts of the combined
apparatus; for the speed and pressure; are illustrated;
to show the principle involved。 While the speed
will give the pressure; it is necessary to make a
calculation to get the result while the machine does
this for you。
_Fig。 61。 Speed Indicator。_
THE SPEED INDICATOR。Four hemispherical
cups A are mounted on four radiating arms B;
which are secured to a vertical stem C; and
adapted to rotate in suitable bearings in a
case; which; for convenience in explaining; is not
shown。
On the lower end of the stem C; is a small bevel
pinion; which meshes with a smaller bevel pinion
within the base。 This latter is on a shaft which
carries a small gear on its other end; to mesh
with a larger gear on a shaft which carries a
pointer D that thus turns at a greatly reduced
speed; so that it can be easily timed。
_Fig。 62。 Air Pressure Indicator。_
AIR PRESSURE INDICATOR。This little apparatus
is readily made of a base A which is provided
with two uprights B; C; through the upper ends of
which are holes to receive a horizontally…disposed
bar D。 One end of the bar is a flat plane
surface E; which is disposed at right angles to the
bar; and firmly fixed thereto。
The other end of the bar has a lateral pin to
serve as a pivot for the end of a link F; its other
end being hinged to the upper end of a lever G;
which is pivoted to the post C; a short distance
below the hinged attachment of the link F; so
that the long end of the pointer which is constituted
by the lever G is below its pivot; and has;
therefore; a long range of movement。
A spring I between the upper end of the pointer
G and the other post B; serves to hold the pointer
at a zero position。 A graduated scale plate J;
within range of the pointer will show at a glance
the pressure in pounds of the moving wind; and
for this purpose it would be convenient to make
the plan