Process for the control of the control surfaces of an aircraft f

Details Process for the control of the control surfaces of an aircraft f Process for the control of the control surfaces of an aircraft f

1993-08-11

1994-12-27

Huppert, Michael S.

Aeronautics and astronautics

Aircraft control

244 76C, 244184, 244 90R, B64C 1300, B64C 1316

Patent

active

053757939

ABSTRACT:
The present invention relates to a process for the automatic control of the control surfaces of an aircraft for the low speed compensation of a lateral path deviation, in which beyond a given deflection threshold (20) of the deflected rudder (17), there is a control of a deflection, proportional to the exceeding of the threshold, of the wing surfaces (13, 14) of one of the two wings (18), said wing being that on the side of the deflected rudder (17), so as to provide a drag supplement to said wing and therefore yaw on the aircraft.
Application to the take-off of large civil transport aircraft.

REFERENCES:
patent: 4146200 (1979-05-01), Borzachillo
patent: 4479620 (1984-10-01), Rogers et al.
patent: 4729528 (1988-03-01), Borzachillo
patent: 4796192 (1989-01-01), Lewis
patent: 4935682 (1990-06-01), McCuen
patent: 5094441 (1992-03-01), Rao
patent: 5112009 (1992-05-01), Farineau
patent: 5186416 (1993-02-01), Fabre et al.

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