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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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5.1 Introduction<br />

5<br />

<strong>The</strong> tail<br />

<strong>Helicopter</strong>s with a single main rotor must have some means <strong>of</strong> balancing <strong>the</strong> torque<br />

reaction due to driving <strong>the</strong> rotor. Whilst <strong>the</strong> anti-torque rotor could be mounted anywhere<br />

for hovering, in forward flight <strong>the</strong> most stable location is aft, supported on some<br />

kind <strong>of</strong> structure called a boom. In addition to <strong>the</strong> anti-torque function helicopters<br />

need some means <strong>of</strong> yaw control and <strong>the</strong> tail rotor also serves that purpose. In order to<br />

balance <strong>the</strong> weight <strong>of</strong> machinery at <strong>the</strong> tail, <strong>the</strong> helicopter cabin usually extends some<br />

way forward <strong>of</strong> <strong>the</strong> mast. This large forward side area is unstable in yaw and generally<br />

some fin area is needed to give directional stability in forward flight. A fur<strong>the</strong>r consideration<br />

is that <strong>the</strong> main rotor on its own is unstable in pitch in forward flight and a<br />

tail plane is usually required.<br />

As a result <strong>the</strong> tail <strong>of</strong> <strong>the</strong> conventional helicopter will be a structure supporting a<br />

variable pitch tail rotor, its transmission and controls, some fin area and a tail plane. In<br />

reality tail booms are also encrusted with antennae, flare launchers, navigation lights,<br />

strobe beacons, static vents, registration letters and warning notices, not to mention<br />

tail skids and occasionally part <strong>of</strong> <strong>the</strong> undercarriage.<br />

In a helicopter with more than one rotor <strong>the</strong> torque may be cancelled in a different<br />

way and a great variety <strong>of</strong> yaw control mechanisms will be found. <strong>The</strong>se multi-rotor<br />

yaw mechanisms are considered in Chapter 9. In this chapter <strong>the</strong> conventional type<br />

<strong>of</strong> tail rotor will be considered, along with a number <strong>of</strong> alternatives having various<br />

advantages and drawbacks. <strong>The</strong> conventional tail rotor is well understood and relatively<br />

inexpensive owing to its wide use.<br />

<strong>The</strong> far aft location <strong>of</strong> <strong>the</strong> tail rotor assembly means that it must be lightly built in<br />

order to avoid <strong>the</strong> machine becoming tail heavy. <strong>The</strong> thrust needed from <strong>the</strong> tail rotor is<br />

much smaller than that needed in <strong>the</strong> main rotor. <strong>The</strong>se two features conspire to ensure<br />

that <strong>the</strong> tail rotor is considerably more fragile than <strong>the</strong> main rotor. Unfortunately <strong>the</strong><br />

fragile tail rotor is in a more exposed location where <strong>the</strong> pilot cannot see it. During<br />

certain manoeuvres, such as quick stops and rearward flight it can get very close to<br />

<strong>the</strong> ground, and it may come <strong>of</strong>f worse in any encounter with vegetation <strong>the</strong> pilot has<br />

not seen. Tail rotor blades are usually fitted with s<strong>of</strong>t aluminium ‘telltales’ at <strong>the</strong> tips<br />

which will be distorted by any impact and indicate that a close inspection for damage<br />

is required.<br />

Generally <strong>the</strong> tail boom will be fitted with some kind <strong>of</strong> skid intended to impact<br />

<strong>the</strong> ground before <strong>the</strong> tail blades. In some cases this is a tubular structure partially<br />

encircling <strong>the</strong> rotor and known as a D-ring. This gives better protection as well as

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