An embodiment includes a system for controlling blade pitch in a rotorcraft having an engine; a drive shaft with a first end and a second end and connected at the first end to the engine; a rotor with two or more blades connected to the second end of the drive shaft; and one or more actuators positioned adjacent to the rotor blades operable to change a blade pitch of the rotor blades.
MAST DAMPENER AND COLLECTIVE PITCH FOR A ROTORCRAFT
2016-09-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
SEMI-AUTOMATIC COLLECTIVE PITCH MECHANISM FOR A ROTORCRAFT
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