G - Physics – 05 – D
Patent
G - Physics
05
D
G05D 1/00 (2006.01)
Patent
CA 2384161
The invention concerns a device for controlling an aircraft manoeuvring components comprising: at least a control member, capable of being actuated by a pilot to deliver manoeuvring commands, at least a central calculating unit (20) adapted to prepare control signals for at least each manoeuvring component based on said manoeuvring commands, each calculating unit being provided with its own failure detecting system. The invention is characterised in that the device further comprises at least a standby electronic module (40), respectively associated with a manoeuvring component, and adapted to likewise prepare control signals for said manoeuvring component based on said manoeuvring commands, said electronic module not being provided with its own failure detecting system, but being connected to a central failure detecting system.
The invention concerns a device for controlling an aircraft manoeuvring components comprising: at least a control member, capable of being actuated by a pilot to deliver manoeuvring commands, at least a central calculating unit (20) adapted to prepare control signals for at least each manoeuvring component based on said manoeuvring commands, each calculating unit being provided with its own failure detecting system. The invention is characterised in that the device further comprises at least a standby electronic module (40), respectively associated with a manoeuvring component, and adapted to likewise prepare control signals for said manoeuvring component based on said manoeuvring commands, said electronic module not being provided with its own failure detecting system, but being connected to a central failure detecting system. Dispositif de commande d'organes de man uvre d'un aéronef comportant: au moins un organe de commande, actionnable par un pilote pour délivrer des ordres de manoeuvre, au moins une unité de calcul centrale (20) apte à établir des signaux de commande pour au moins un organe de man uvre à partir desdits ordres de manoeuvre, chaque unité de calcul centrale étant pourvue d'un système de détection de panne propre. Conformément à l' invention, le dispositif comporte en outre au moins un module électronique de secours (40), associé respectivement à un organe de manoeuvre, et apte à établir également des signaux de commande pour cet organe de manoeuvre à partir desdits ordres de manoeuvre, ledit module électronique étant dépourvu de système de détection de panne propre, mais relié à un système central de détection de panne.
Garcia Jean-Pierre
Ortega Jean-Marc
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
LandOfFree
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