Dual control mechanism for aircraft

Details Dual control mechanism for aircraft Dual control mechanism for aircraft

1993-02-24

1995-06-27

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft control

Pilot operated

244234, 74471R, 74493, B64C 1312

Patent

active

054273366

ABSTRACT:
A control mechanism for aircraft having a vertically extending, short stub with a cross bar attached to its upper end and a pair of arcuate lower members extending from the cross bar toward the forward end of the aircraft with an adjustable positioning arm on each lower member extending rearwardly and which mounts a hand grip for controlling the aircraft. In a single control mechanism, one arcuate lower member is attached directly to the stub.

REFERENCES:
patent: D135167 (1943-03-01), Obszarny
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: 1874522 (1932-08-01), Henrichsen
patent: 2272817 (1942-02-01), Palmer
patent: 3228478 (1966-01-01), Edenborough
patent: 3271045 (1966-09-01), Vacante
patent: 3941009 (1976-03-01), Brown
patent: 3994453 (1976-11-01), Firestone
patent: 4114843 (1978-09-01), Robinson
patent: 4726311 (1988-02-01), Niina
patent: 4811921 (1989-03-01), Whitaker et al.
patent: 4887782 (1989-12-01), Carnell et al

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