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Arrangement for controlling of rotor blades of helicopter has controlled actuator, for collective and cyclic adjustment of blade setting angle of rotor blades, which are mechanically forcibly coupled among themselves
Arrangement for controlling of rotor blades of helicopter has controlled actuator, for collective and cyclic adjustment of blade setting angle of rotor blades, which are mechanically forcibly coupled among themselves
Arrangement has controlled actuator (3), for collective and cyclic adjustment of blade setting angle of rotor blades (1), which are connected with rotor blade in such a way that its longitudinal axis runs parallel to the longitudinal axis (4) of the rotor blade. Actuators are mechanically forcibly coupled among themselves.
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