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

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 13/24 (2006.01) B64C 13/42 (2006.01) B64C 13/50 (2006.01) G05D 1/00 (2006.01)

Patent

CA 2185299

The device has at least two servo-systems, each having at least one electric control input. At least one of the servo-systems, called the mixed servo-system, also has a mechanical control input, and an electric control system for the servo-systems is able to occupy a state corresponding to a fault of an engine in which at least two of the servo-systems simultaneously operate the rudder and a state corresponding to an electric fault, in which the mixed servo-system operates the controlled rudder from the mechanical control input.

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