| 摘要 |
<p>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.</p> |
