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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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O<strong>the</strong>r types <strong>of</strong> rotorcraft 369<br />

Fig. 9.21 <strong>The</strong> Dogship was Piasecki’s first tandem rotor helicopter and was widely demonstrated to attract<br />

interest in <strong>the</strong> principle. It was <strong>the</strong> forerunner <strong>of</strong> <strong>the</strong> ‘flying bananas’ and <strong>the</strong> Chinook. (Boeing)<br />

Fig. 9.22 <strong>The</strong> transmission system <strong>of</strong> <strong>the</strong> Chinook showing <strong>the</strong> synchronizing shaft between <strong>the</strong> rotors and<br />

<strong>the</strong> twin engines.<br />

Chapter 5 described <strong>the</strong> interaction between <strong>the</strong> main and tail rotor <strong>of</strong> a conventional<br />

helicopter. In <strong>the</strong> hover it was seen to be highly variable with wind direction, whereas<br />

in translational flight <strong>the</strong>re was a beneficial wea<strong>the</strong>rcocking effect. In <strong>the</strong> tandem <strong>the</strong><br />

interference between <strong>the</strong> two rotors in <strong>the</strong> hover is beneficially almost independent <strong>of</strong><br />

wind direction, whereas in forward flight it is detrimental to stability. Consequently it<br />

is simplistic to claim that one configuration is better than ano<strong>the</strong>r. In some areas <strong>the</strong><br />

conventional approach is superior, but in o<strong>the</strong>r areas <strong>the</strong> tandem wins.<br />

Figure 9.22 shows <strong>the</strong> transmission arrangement <strong>of</strong> <strong>the</strong> CH-47 (Chinook) in which<br />

<strong>the</strong> two engines drive <strong>the</strong> synchronizing shaft via one-way clutches so that ei<strong>the</strong>r engine<br />

can drive both rotors. It is interesting to note that except for <strong>the</strong> use <strong>of</strong> piston engines,<br />

<strong>the</strong> Florine III <strong>of</strong> 1935 had <strong>the</strong> same transmission layout. As <strong>the</strong> dominant masses and<br />

<strong>the</strong> rotor forces are both concentrated at <strong>the</strong> ends <strong>of</strong> <strong>the</strong> hull, <strong>the</strong> structure needs to be<br />

stiff against bending and torsion. <strong>The</strong> loss <strong>of</strong> disc area due to <strong>the</strong> overlap <strong>of</strong> <strong>the</strong> two

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