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The Art of the Helicopter John Watkinson - Karatunov.net

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28 <strong>The</strong> <strong>Art</strong> <strong>of</strong> <strong>the</strong> <strong>Helicopter</strong><br />

2.6 Moments and couples<br />

So far only forces that all conveniently act at one point have been considered. In reality<br />

forces can also act at a distance from a point. When a force does not pass through a point<br />

<strong>the</strong> result is called a moment with respect to that point. <strong>The</strong> moment is equal to <strong>the</strong> force<br />

multiplied by <strong>the</strong> distance at right angles to <strong>the</strong> force, as shown in Figure 2.7. Applying<br />

a moment to an object will cause it to turn and accelerate along simultaneously.<br />

If two equal and opposite forces act a distance apart, <strong>the</strong> result is a pure turning<br />

effort known as a couple or as torque. A helicopter engine produces a couple at <strong>the</strong><br />

output shaft in order to drive <strong>the</strong> blades. <strong>The</strong> reaction to this couple attempts to twist<br />

<strong>the</strong> engine against its mountings. <strong>The</strong> transmission conveys <strong>the</strong> engine power to <strong>the</strong><br />

rotor shaft. <strong>The</strong> rotor shaft exerts a couple on <strong>the</strong> rotor head in order to drive <strong>the</strong><br />

blades round. <strong>The</strong> torque reaction to this couple attempts to rotate <strong>the</strong> transmission,<br />

and <strong>the</strong> helicopter hanging from it, <strong>the</strong> opposite way. One <strong>of</strong> <strong>the</strong> jobs <strong>of</strong> <strong>the</strong> designer is<br />

to find a means to prevent this rotation.<br />

When a body is supported at <strong>the</strong> CM, it will remain in <strong>the</strong> initial attitude. Figure 2.8<br />

shows that if <strong>the</strong> support is not at <strong>the</strong> CM, <strong>the</strong> body will rotate. It may swing from side<br />

to side, but eventually will come to rest with <strong>the</strong> CM below <strong>the</strong> point <strong>of</strong> support.<br />

It is <strong>of</strong>ten assumed that <strong>the</strong> CM <strong>of</strong> <strong>the</strong> helicopter is below <strong>the</strong> rotor shaft, but this<br />

may not be <strong>the</strong> case. Figure 2.9 shows how a helicopter hovers with <strong>the</strong> CM displaced.<br />

<strong>The</strong> CM tends to hang directly beneath <strong>the</strong> rotor head, and <strong>the</strong> pilot has to displace<br />

<strong>the</strong> cyclic control in order to keep <strong>the</strong> disc horizontal so <strong>the</strong> rotor thrust vector is<br />

straight up. Clearly if <strong>the</strong> CM is a long way from <strong>the</strong> mast, a substantial amount <strong>of</strong><br />

cyclic control will be used up to compensate, and <strong>the</strong>re may not be enough left to<br />

control <strong>the</strong> machine. In addition <strong>the</strong> bearings and joints in <strong>the</strong> rotor head find it harder<br />

to transmit power when <strong>the</strong> shaft and <strong>the</strong> disc are not aligned.<br />

Fig. 2.7 (a) A moment about a point is <strong>the</strong> product <strong>of</strong> <strong>the</strong> force and <strong>the</strong> distance. (b) A pure couple results from<br />

two equal and opposite forces that do not coincide.

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