Aircraft control system providing hardover protection and full c

Details Aircraft control system providing hardover protection and full c Aircraft control system providing hardover protection and full c

1976-08-05

1978-04-04

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft, heavier-than-air

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

244177, 244194, B64C 1302

Patent

active

040822389

ABSTRACT:
In a helicopter a servo system connected to operate in parallel with the rotor blade pitch controlling linkages and also to receive autopilot generated signals directing maneuvers. The system limits the autopilot control over the blade pitch or position in the short term and permits full control over the long term.

REFERENCES:
patent: 3528633 (1970-09-01), Knemeyer
patent: 3920966 (1975-11-01), Knemeyer et al.
patent: 3935523 (1976-01-01), Cleveland et al.

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