Aircraft flight control system

Aeronautics and astronautics – Aircraft control

Patent

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Details

91464, 91509, B64C 900

Patent

active

047445327

ABSTRACT:
Flight control system for aircraft of the type provided with ailerons, elevators, upper surface spoilers, and upper surface air-brakes, a rudder and horizontal stabilizers with variable angle of incidence, said system comprising an electric control, in some cases without any mechanical emergency control for said upper surface spoilers and air-brakes.
According to the invention:

REFERENCES:
patent: 3062192 (1962-11-01), Webb
patent: 3190185 (1965-06-01), Rasmussen
patent: 3295420 (1967-01-01), Gleason
patent: 3338138 (1967-08-01), Wood
patent: 3529514 (1969-03-01), Mayo et al.
patent: 3683749 (1972-08-01), Boyles
patent: 4394999 (1983-07-01), Botzler
patent: 4472780 (1984-09-01), Chenoweth et al.

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