Command process and system for an aircraft control surface...

B - Operations – Transporting – 64 – C

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B64C 13/40 (2006.01) B64C 13/42 (2006.01) B64C 13/50 (2006.01)

Patent

CA 2293166

Système de commande d'une gouverne (100) d'un aéronef comprenant au moins un actionneur (102, 104) de la gouverne, relié à un circuit hydraulique et équipé d'au moins deux vérins de puissance (110) aptes à fonctionner selon au moins un mode activé et un mode désactivé. Conformément à l'invention, le système comporte en outre une unité de commande (114) apte à faire fonctionner dans un mode activé un nombre de vérins fonction des conditions de vol de l'aéronef. Application aux avions.

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