Helicopter flight control systems

Details Helicopter flight control systems Helicopter flight control systems

1987-12-10

1989-05-30

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft, heavier-than-air

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

B64C 2757

Patent

active

048343188

ABSTRACT:
In a helicopter, signals representative of the rotor disc attitude of a main sustaining rotor (11) are fed into a flight control system (24) to modify an actuator demand signal (31) controlling a rotor blade actuation system (32) of the main sustaining rotor.

REFERENCES:
patent: 3938762 (1976-02-01), Murphy
patent: 3954229 (1976-05-01), Wilson
patent: 4025230 (1977-05-01), Rastan
patent: 4519743 (1985-05-01), Ham

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