Tandem rotor wing rotational position control system

Details Tandem rotor wing rotational position control system Tandem rotor wing rotational position control system

2004-09-14

2009-06-16

Mansen, Michael R (Department: 3644)

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

C244S195000, C244S012300, C244S006000, C244S017230, C244S207000

Reexamination Certificate

active

07546975

ABSTRACT:
A rotational position-adjusting system (6) for a vertical takeoff and landing aircraft (4). The system (6) includes multiple detectors (60) that generate rotor signals. The rotor signals are indicative of the position of each rotor (8) of the aircraft (4). The rotors (8) provide lift to the aircraft (4). A controller (24) is coupled to the detectors (60) and adjusts the rotational speed of one or more of the rotors (8) in response to the rotor signals.

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