Aircraft flight control system

Machine element or mechanism – Control lever and linkage systems – Multiple controlling elements for single controlled element

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Details

64 28R, 137 71, 416 2, 416114, G05G 1100

Patent

active

041214838

ABSTRACT:
An aircraft flight control including a linkage system having a walking beam to which control inputs are imparted and from which a control output is taken and having anti-jamming and over-control abatement provisions.

REFERENCES:
patent: 1311774 (1919-07-01), Ritter
patent: 3103004 (1963-09-01), Murray
patent: 3119636 (1964-01-01), Kummerman
patent: 3128738 (1964-04-01), Farrington et al.

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