Helicopter control device

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244 1725, 74471XY, B64C 2758

Patent

active

041345606

ABSTRACT:
A helicopter control system for controlling cyclic pitch, collective pitch, throttle and rudder. A handle is secured to a vertical shaft slidable or telescopic within a cylindrical tube. A locking device permits the tube and shaft to be moved as a unit to control cyclic pitch. Vertical movement of the shaft controls collective pitch. Rotation of the shaft controls the tail rotor. A twist-grip on the handle is provided for throttle control. The handle may be adjusted through a ball joint for pilot comfort.

REFERENCES:
patent: 1190374 (1916-07-01), Capdevila
patent: 2076088 (1937-04-01), Malinowski
patent: 2386709 (1945-10-01), Osborn
patent: 2460374 (1949-02-01), Walls
patent: 2505020 (1950-04-01), Weisman
patent: 3350956 (1967-11-01), Monge
patent: 3543599 (1970-12-01), Caswell
patent: 3971536 (1976-07-01), Rollins, Jr.
patent: 4062508 (1977-12-01), Stephens et al.

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