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UNI-Mechanics 2000
13. A few basic terms used in model helicopter flying
The term „rotary wing machine" indicates that the helicopter's lift is derived from rotating „wings"
which take the form of rotor blades. As a result, a helicopter does not require a minimum
forward speed in order to fly, i.e. it can hover.
13.1 Cyclic pitch
Cyclic pitch variation is used to steer the machine around the roll and pitch axes. Changing
cyclic pitch has the effect of altering blade pitch depending on its position in the circle. The
effect is caused by tilting the swashplate, which then effectively tilts the helicopter in the
required direction.
13.2 Collective pitch
Collective pitch provides control over vertical movement, i.e. for climb and descent. The pitch of
both rotor blades is altered simultaneously.
13.3 Torque compensation
The spinning rotor produces a torque moment which tends to turn the whole helicopter in the
opposite direction. This effect must be accurately neutralised, and that is the purpose of the tail
rotor. Tail rotor blade pitch is altered to vary torque compensation. The tail rotor is also used to
control the model around the vertical (yaw) axis.
13.4 Hovering
This is the state in which the helicopter flies in a fixed position in the air, without moving in any
direction.
13.5 Ground effect
Ground effect is a phenomenon which only occurs when the machine is close to the ground,
and it falls off as altitude rises. At an altitude of about 1 - 1.5 times the rotor diameter, ground
effect is completely absent. Normally the revolving airflow from the main rotor is able to flow
away freely, but in ground effect the air strikes a fixed obstacle (the ground) and forms an „air
cushion". In ground effect a helicopter can lift more weight, but its positional stability is reduced,
with the result that it tends to „break away" unpredictably in any direction.
13.6 Climb
Any excess power above that required for hovering can be exploited to make the helicopter
climb. Note that a vertical climb requires more energy than an angled climb, i.e. one which
includes forward motion. For this reason a model with a given amount of motor power will climb
more rapidly at an angle than vertically.
13.7 Level flight
A helicopter absorbs least power when flying straight and level at about half-power. If you have
trimmed the machine carefully for a steady hover, it will tend to turn to one side when flown
forward. The reason for this phenomenon is that the rotor blade which is moving forward
encounters an increased airflow caused by the wind, and this increases its upthrust compared
with the blade which is moving downwind, where the same airflow has to be subtracted. The net
result is a lateral inclination of the helicopter.
13.8 Descent
If the helicopter's rotor speed is relatively low and you place the helicopter in a fast vertical
descent, the result may be that insufficient air flows through the rotor. This can cause what is
known as a „turbulence ring", i.e. the airflow over the blade airfoil breaks away. The helicopter is
then uncontrollable and will usually crash. A high-speed descent is therefore only possible if the
helicopter is moving forward, or if the rotor is spinning at high speed. For the same reason care
should be exercised when turning the model helicopter downwind after flying into wind.
13.9 Flapping motion of the rotor blades
As we have already seen, the forward-moving blade produces greater upthrust than the other
blade. This effect can be minimised by allowing the forward-moving blade to rise and the other
blade to fall. The rotor head is fitted with what is known as a flapping hinge to allow this
movement, and this prevents the rotor plane tilting excessively in forward flight. In model
helicopters a single hinge shared by both blades has proved a good solution to the problem.
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