Helicopter rotor control systems

Details Helicopter rotor control systems Helicopter rotor control systems

1987-06-08

1989-02-21

Barefoot, Galen

Aeronautics and astronautics

Aircraft, heavier-than-air

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

416163, B64C 2754

Patent

active

048058505

ABSTRACT:
A helicopter rotor control system includes a plurality of control rods (31) extending downwardly from pitch control means (24) through a hollow rotor drive shaft (12) and gearbox (14) for connection directly to individual actuators (36) located generally concentrically of an axis of rotation (15).

REFERENCES:
patent: 1052378 (1913-02-01), Porter
patent: 2664168 (1953-12-01), Giroz

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