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Individual blade control for a helicopter main rotor with additional separate collective blade control
Individual blade control for a helicopter main rotor with additional separate collective blade control
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机译：直升机主旋翼的单独桨叶控制，以及额外的单独集体桨叶控制
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摘要
The individual blade control device is for a helicopter rotor which has a rotationally driven rotor mast (2), a rotor hub (4) and several rotor blades (6,8,10,12) installed around the circumference of the hub, whereby means are provided for the mechanical transmission of exclusively collective control movements from a non-rotating system into a rotating system, the control movements of which in the rotating system are superimposed on the control movements of the individual actuators (16). An independent claim is included for a method for the control of a helicopter with an individual rotor blade control device.
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