CHAPTER IX.

THE STEERING OF THE MODEL.

§ 1. Of all the various sections of model aeroplaning that which is

the least satisfactory is the above.

The torque of the propeller naturally exerts a twisting or tilting

effect upon the model as a whole, the effect of which is to cause it

to fly in (roughly speaking) a circular course, the direction

depending on whether the pitch of the screw be a right or left handed

one. There are various devices by which the torque may be

(approximately) got rid of.

§ 2. In the case of a monoplane, by not placing the rod carrying the

rubber motor in the exact centre of the main aerofoil, but slightly to

one side, the exact position to be determined by experiment.

In a biplane the same result is obtained by keeping the rod in the

centre, but placing the bracket carrying the bearing in which the

propeller shaft runs at right angles horizontally to the rod to obtain

the same effect.

§ 3. The most obvious solution of the problem is to use _two_ equal

propellers (as in the Wright biplane) of equal and opposite pitch,

driven by two rubber motors of equal strength.

Theoretically this idea is perfect. In practice it is not so. It is

quite possible, of course, to use two rubber motors of an equal number

of strands (equality should be first tested by _weighing_). It should

be possible to obtain two propellers of equal and opposite pitch,

etc., and it is also possible to give the rubber motors the same

number of turns. In practice one is always wound up before the other.

This is the first mistake. They should be wound up _at the same time_,

using a double winder made for the purpose.

The fact that this is _not_ done is quite sufficient to give an

unequal torsion. The friction in both cases must also be exactly

equal. Both propellers must be released at exactly the same instant.

Supposing _all_ these conditions fulfilled (in practice they never

are), supposing also the propellers connected by gearing (prohibitive

on account of the weight), and the air quite calm (which it never is),

then the machine should and undoubtedly would _fly straight_.

For steering purposes by winding up one propeller _many more times_

than the other, the aeroplane can generally speaking be steered to the

right or left; but from what I have both seen and tried twin-screw

model aeroplanes are _not_ the success they are often made out to be,

and they are much more troublesome to deal with, in spite of what some

say to the contrary.

The solution of the problem of steering by the use of two propellers

is only partially satisfactory and reliable, in fact, it is no

solution at all.[45] The torque of the propeller and consequent

tilting of the aeroplane is not the only cause at work diverting the

machine from its course.

§ 4. As it progresses through the air it is constantly meeting air

currents of varying velocity and direction, all tending to make the

model deviate more or less from its course; the best way, in fact, the

only way, to successfully overcome such is by means of _speed_, by

giving the aeroplane a high velocity, not of ten or twelve to fifteen

miles an hour, as is usual in built up fabric-covered aerofoils, but a

velocity of twenty to thirty miles an hour, attainable only in models

(petrol or steam driven) or by means of wooden or metal aerofoils.

§ 5. Amongst devices used for horizontal steering are vertical "FINS."

These should be placed in the rear above the centre of gravity. They

should not be large, and can be made of fabric tightly stretched over

a wire frame, or of a piece of sheet magnalium or aluminium, turning

on a pivot at the front edge, adjustment being made by simply twisting

the fin round to the desired angle. As to the size, think of rudder

and the size of a boat, but allow for the difference of medium. The

frame carrying the pivot and fin should be made to slide along the rod

or backbone of the model in order to find the most efficient position.

§ 6. Steering may also be attempted by means of little balancing tips,

or ailerons, fixed to or near the main aerofoil, and pivoted (either

centrally or otherwise) in such a manner that they can be rotated one

in one direction (tilted) and the other in the other (dipped), so as

to raise one side and depress the other.

§ 7. The model can also be steered by giving it a cant to one side by

weighting the tip of the aerofoil on that side on which it is desired

it should turn, but this method is both clumsy and "weighty."

§ 8. Another way is by means of the elevator; and this method, since

it entails no additional surfaces entailing extra resistance and

weight, is perhaps the most satisfactory of all.

It is necessary that the elevator be mounted on some kind of universal

joint, in order that it may not only be "tipped" or "dipped," but also

canted sideways for horizontal steering.

§ 9. A vertical fin in the rear, or something in the nature of a

"keel," i.e. a vertical fin running down the backbone of the machine,

greatly assists this movement.

If the model be of the tractor screw and tail (Blériot) type, then the

above remarks _re_ elevator apply _mutatis mutandis_ to the tail.

§ 10. It is of the most vital importance that the propeller torque

should be, as far as possible, correctly balanced. This can be tested

by balancing the model transversely on a knife edge, winding up the

propeller, and allowing it to run down, and adjusting matters until

the torque and compensatory apparatus balance. As the torque varies

the mean should be used.

In the case of twin propellers, suspend the model by its centre of

gravity, wind up the propellers, and when running down if the model is

drawn forward without rotation the thrust is equal; if not adjustment

must be made till it does. The easiest way to do this _may_ be by

placing one propeller, the one giving the greater thrust, slightly

nearer the centre.

In the case of two propellers rotating in opposite directions (by

suitable gearing) on the common centre of two axes, one of the axes

being, of course, hollow, and turning on the other--the rear propeller

working in air already driven back by the other will require a coarser

pitch or larger diameter to be equally efficient.

FOOTNOTE:

[45] These remarks apply to rubber driven motors. In the case of

two-power driven propellers in which the power was automatically

adjusted, say, by a gyroscope as in the case of a torpedo--and the

_speed_ of each propeller varied accordingly--the machine could, of

course, be easily steered by such means; but the model to carry such

power and appliances would certainly weigh from 40 lb. to 60 lb.

The Theory and Practice of Model Aeroplaning · 第 7 / 12 章