Control system for aircraft

Details Control system for aircraft Control system for aircraft

B - Operations, Transporting

64

C

B64C 13/12 (2006.01) G06F 19/00 (2006.01) G09B 9/46 (2006.01)

Patent

CA 2156928

A control mechanism for aircraft (70) having a vertically extending member (72) with a cross bar (74) attached to its upper end and a pair of arcuate lower members (76) extending from the cross bar (74) toward the forward end of the aircraft with an adjustable positioning arm (84) on each lower member (76) extending rearwardly and which mounts a hand grip (86) for controlling the aircraft. The mechanism includes a damping system with a frame (205) connected to the cross bar (74) with bearing elements (230).

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