Control stick assembly

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

74492, 74543, 244 83F, 180 77C, B64C 1312

Patent

active

041148436

ABSTRACT:
A control stick assembly for dual control of aircraft includes a single control stick for longitudinal and lateral orientation of the aircraft. The stick is mounted on the center of the aircraft by a joint permitting lateral and longitudinal movement by a crossbar mounted on the stick. The crossbar is hinged vertically above the joint and is tiltable freely in a vertical plane. Grips are mounted on crossbar and located in front of each of the pilot and copilot so that each may control the aircraft through a single stick. The stick is connected to appropriate linkages to move the ailerons and elevator of an airplane or the rotor blades of a helicopter.

REFERENCES:
patent: D135167 (1943-03-01), Obszarny et al.
patent: 792573 (1905-06-01), Duryea
patent: 1798724 (1931-03-01), Chalmers
patent: 1807939 (1931-06-01), Sikorsky
patent: 1855988 (1932-04-01), Ranasey
patent: 3228478 (1966-01-01), Edenborough
patent: 3271045 (1966-09-01), Vacante
patent: 3994453 (1976-11-01), Firestone

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