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The Art of the Helicopter John Watkinson - Karatunov.net

The Art of the Helicopter John Watkinson - Karatunov.net

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

that weights are added at various places along <strong>the</strong> axis to bring <strong>the</strong> CM <strong>of</strong> <strong>the</strong> slices<br />

onto <strong>the</strong> axis. When balancing car wheels, note that weights may be fitted both to <strong>the</strong><br />

inner and outer rims to achieve this.<br />

In <strong>the</strong> case <strong>of</strong> a helicopter rotor, <strong>the</strong> blades will be in <strong>the</strong> same plane and so <strong>the</strong> effects<br />

due to Figure 2.19(b) will be small. However, a statically balanced rotor could still be<br />

achieved if one blade were heavier than <strong>the</strong> o<strong>the</strong>r, if its CM were nearer <strong>the</strong> shaft. Thus<br />

to dynamically balance a rotor, it is necessary that all <strong>of</strong> <strong>the</strong> blades should have exactly<br />

<strong>the</strong> same mass, and <strong>the</strong> same radius <strong>of</strong> gyration. This means that <strong>the</strong> distribution<br />

<strong>of</strong> mass along and across each blade should be identical and <strong>the</strong> CM should be at <strong>the</strong><br />

same point in three axes. In full size rotor blades, weight pockets are provided at various<br />

places to allow <strong>the</strong>se conditions to be met.<br />

In model helicopters dynamic balancing is just as important, but a simplified<br />

approach can be used. Figure 2.19(c) shows that <strong>the</strong> blades must be carefully weighed,<br />

and a piece <strong>of</strong> covering material is cut to have exactly <strong>the</strong> same mass as <strong>the</strong> difference<br />

in masses <strong>of</strong> <strong>the</strong> blades. <strong>The</strong> blades are assembled to <strong>the</strong> balanced rotor head, and<br />

<strong>the</strong> covering material is applied to <strong>the</strong> lighter blade at a point where static balance is<br />

achieved. It will <strong>the</strong>n be found that <strong>the</strong> two blades have <strong>the</strong>ir CM in <strong>the</strong> same place and<br />

so <strong>the</strong> rotor will be dynamically balanced. <strong>The</strong> same result will be obtained if <strong>the</strong> covering<br />

is moved until both blades balance in <strong>the</strong> same place. In full-size helicopters<br />

<strong>the</strong> leading edge <strong>of</strong> <strong>the</strong> blade may be protected with a replaceable plastic film. If<br />

part <strong>of</strong> this comes <strong>of</strong>f or <strong>the</strong> film is not fitted identically to each blade, vibration<br />

may result.<br />

2.12 <strong>The</strong> mechanics <strong>of</strong>rotation<br />

Figure 2.20(a) shows a steady rotation which could be a mass te<strong>the</strong>red by a string.<br />

Tension in <strong>the</strong> string causes an inward force that accelerates <strong>the</strong> mass into a circular<br />

path. <strong>The</strong> tension can be described as a rotating vector. When viewed from <strong>the</strong> side,<br />

<strong>the</strong> displacement about <strong>the</strong> vertical axis appears sinusoidal. <strong>The</strong> vertical component<br />

<strong>of</strong> <strong>the</strong> tension is also sinusoidal, and out <strong>of</strong> phase with <strong>the</strong> displacement. As <strong>the</strong> two<br />

parameters have <strong>the</strong> same waveform, <strong>the</strong>y must be proportional. In o<strong>the</strong>r words <strong>the</strong><br />

restoring force acting on <strong>the</strong> mass is proportional to <strong>the</strong> displacement.<br />

Fig. 2.20 (a) A te<strong>the</strong>red mass is moving in a circle. If <strong>the</strong> component <strong>of</strong> this motion in one axis only is resolved,<br />

<strong>the</strong> motion will be found to be <strong>the</strong> same as a mass supported on a spring, (b).

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