Redundant flight control system

F - Mech Eng,Light,Heat,Weapons – 16 – H

Patent

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244/66

F16H 21/44 (2006.01) B64C 13/30 (2006.01)

Patent

CA 1094037

REDUNDANT FLIGHT CONTROL SYSTEM ABSTRACT OF THE DISCLOSURE A flight control system utilizing pilot actuated flexible cables to selectively move a control quadrant and utilizing balanced, preloaded springs connected to the quadrant to be selectively automatically releasable in response to cable severance so that the quadrant can be pilot actuated through its full control regime despite the severance of one of the cables. -1-

312066

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