System for controlling an aircraft control surface tab

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244228, 244195, 244 76A, B64C 904, B64C 910

Patent

active

059134925

ABSTRACT:
A system for controlling the tab (6) of an aircraft control surface (3) having a pair of position sensors (12 and 15) that supply information regarding the turning of the control surface (3) and the position of a jack (13), respectively, on the basis of signals generated by the sensors (12 and 15) as well as possibly on the basis of at least one parameter (p) originating from the aircraft, such as airspeed, positions of lift-augmenting devices, forces exerted by the pilot on a control, etc., and which formulates a command for the jack (13).

REFERENCES:
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patent: 2557426 (1951-06-01), George
patent: 2563757 (1951-08-01), Thorp
patent: 2568719 (1951-09-01), Curry, Jr.
patent: 2577439 (1951-12-01), Wendt
patent: 2640665 (1953-06-01), Gibb
patent: 2719684 (1955-10-01), Peed, Jr.
patent: 2721716 (1955-10-01), Meredith
patent: 2817483 (1957-12-01), Hill
patent: 4595458 (1986-06-01), Robinson
patent: 4765572 (1988-08-01), Bellego et al.
French Search Report, 3 pages, dated Feb. 3, 1997.

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