Process and device for the control of the rudder of an aircraft

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244227, 244235, 244236, B64C 1342

Patent

active

057915962

ABSTRACT:
A device for controlling a rudder of an aircraft has at least two servo-systems each including at least one electric control input. At least one of the servo-systems is a mixed servo-system that also has a mechanical control input. When an engine fault occurs, an electric control system causes at least two of the servo-systems to simultaneously operate the rudder. When the electric control system is not operational due to an electric fault, the mixed servo-system operates the rudder based on control signals from the mechanical control input.

REFERENCES:
patent: 4759515 (1988-07-01), Carl
patent: 4762294 (1988-08-01), Carl
patent: 4765568 (1988-08-01), Carl et al.
patent: 4793576 (1988-12-01), Frerk
patent: 4905933 (1990-03-01), Ako

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