Control system for aircraft

Aeronautics and astronautics – Aircraft control – Pilot operated

Patent

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Details

244234, B64C 1312

Patent

active

055270042

ABSTRACT:
A control mechanism for aircraft having a vertically extending, member 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. The mechanism includes a damping system with a frame connected to the crossbar with bearing elements.

REFERENCES:
patent: D135167 (1942-11-01), 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: 1874522 (1932-08-01), Henrichsen
patent: 2272817 (1942-02-01), Palmer
patent: 3228478 (1966-01-01), Edenborough
patent: 3271045 (1966-09-01), Vacante
patent: 3785596 (1974-01-01), Chinchester-Miles
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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