Low latency pitch adjustable rotors are disclosed. A disclosed example rotor includes a rotor hub to rotate about a rotational axis, rotor blades coupled to the rotor hub, the rotor blades being pitch adjustable and having corresponding pitch angles, and a reaction hinge operatively coupled between the rotor hub and the rotor blades, the reaction hinge to move relative to the rotor hub in response to an angular acceleration or deceleration of the rotor hub to adjust the pitch angles.
LOW LATENCY PITCH ADJUSTABLE ROTORS
2020-10-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |