B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 41/00 (2006.01) B64C 25/24 (2006.01) H02J 4/00 (2006.01)
Patent
CA 2688818
The invention relates to a power distribution architecture for an aircraft for powering aircraft electromechanical actuators, the architecture comprising at least one power distribution member for distributing power to such and such an electromechanical actuator connected to the architecture, the architecture receiving power from at least one power supply bus of the aircraft. According to the invention, a DC network of voltage that is variable in controlled manner is interposed between the power supply bus of the aircraft and the power distribution members.
L'invention est relative à une architecture de distribution de puissance pour aéronef, destinée à alimenter des actionneurs électromécaniques d'aéronefs, l'architecture comportant au moins un organe de distribution de puissance pour distribuer la puissance à tel ou tel actionneur électromécanique relié à l'architecture, l'architecture recevant la puissance d'au moins un bus d'alimentation en puissance de l'aéronef. Selon l'invention, un réseau à tension continue variable de façon commandée est interposé entre le bus d'alimentation en puissance de l'aéronef et les organes de distribution de puissance.
Leynaert Francois-Noel
Nierlich Florent
Goudreau Gage Dubuc
Messier-Bugatti
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