Redundant flight control system

Machine element or mechanism – Control lever and linkage systems – Hand operated

Patent

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Details

74470, 244 83K, B64C 1304, F16C 110

Patent

active

041866223

ABSTRACT:
A flight control system utilizing pilot actuated flexible cables to selectively move a control quadrant and utilizing preloaded bungees additionally connecting each cable to the quadrant so that the quadrant can be pilot actuated despite the severance of one of the cables.

REFERENCES:
patent: 2581080 (1952-01-01), Cushman
patent: 2810300 (1957-10-01), Pigford
patent: 2841030 (1958-07-01), Wrighton
patent: 2856790 (1958-10-01), Norton
patent: 2865224 (1958-12-01), Krouse
patent: 3199601 (1965-08-01), Dean et al.
patent: 3277738 (1966-10-01), Glauser et al.
patent: 3316775 (1967-05-01), Wrighton et al.
patent: 3473407 (1969-10-01), Hicks
patent: 3532302 (1970-10-01), Dean
patent: 3919897 (1975-11-01), Yang

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