System for automatically controlling an aircraft's high-lift...

B - Operations – Transporting – 64 – C

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B64C 13/20 (2006.01) G05D 1/00 (2006.01)

Patent

CA 2472291

-A control system (1) that includes an actuation section (14) that moves lift-enhancing devices (12, 13), a control member (16), and a control unit (17) that includes a control section (18) that produces control orders, as a function of actuation of the control member (16), so as to control the actuation section (14); a control unit (19) that produces automatically auxiliary control orders which are transmitted to the actuation section (14 )to automatically retract the lift-enhancing devices (12, 13) when the aircraft (2) is in a first flight condition and another device (20) that automatically disables control orders (18) to deploy the lift-enhancing devices (12, 13) when the aircraft (2) is in a second flight condition.

- Le système (1) comporte des moyens d'actionnement (14) pour déplacer des dispositifs hypersustentateurs (12, 13), un organe de commande (16), et une unité de commande (17) comportant un moyen de commande (18) engendrant des ordres en fonction de l'actionnement dudit organe de commande (16) pour commander les moyens d'actionnement (14), un dispositif (19) engendrant des ordres auxiliaires transmis aux moyens d'actionnement (14) pour rétracter automatique- ment les dispositifs hypersustentateurs (12, 13), lorsque l'aéronef (2) se trouve dans une première condition de vol, et un dispositif (20) pour inhiber des ordres engendrés par le moyen de commande (18) pour déployer les dispositifs hypersustentateurs (12, 13), lorsque l'aéronef (2) se trouve dans une seconde condition de vol.

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