Redundant flight control system

Machine element or mechanism – Mechanical movements – Oscillating to oscillating

Patent

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Details

244232, 244 83K, 74501R, F16H 2144

Patent

active

041701470

ABSTRACT:
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.

REFERENCES:
patent: 1996332 (1935-04-01), Grinslale
patent: 2304487 (1942-12-01), Stinson
patent: 2430869 (1947-11-01), Fulton, Jr.
patent: 2669401 (1954-02-01), Bosserman
patent: 2778455 (1957-01-01), Roach
patent: 3031036 (1962-04-01), Meyers

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