Distributed flight control system implemented according to...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 13/50 (2006.01)

Patent

CA 2754031

The invention relates to a flight control system for an aircraft, intended for controlling a plurality of actuators adapted for actuating the control surfaces of said aircraft from information supplied by the piloting members and/or sensors of the aircraft. The system includes a primary control system (SYSTP) adapted for controlling a first set of control surface actuators and a secondary control system (SYSTS) adapted for controlling a second set of control surface actuators, the primary and secondary systems being respectively powered by independent energy sources (Ep, Es) of different types.

L'invention concerne un système de commande de vol pour aéronef, destiné à commander une pluralité d'actionneurs adaptés à actionner des gouvernes du dit aéronef à partir d'informations fournies par les organes de pilotage et/ou des capteurs de l'aéronef. Le système comprend un système de commande primaire (SYSTP) adapté à contrôler un premier ensemble d'actionneurs de gouvernes et un système de commande secondaire (SYSTS) adapté à contrôler un second ensemble d'actionneurs de gouvernes, les systèmes primaire et secondaire étant respectivement alimentés par des sources d'énergie (Ep, Es) indépendantes et de types différents.

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