Fadec and avionic component distributed architecture

Details Fadec and avionic component distributed architecture Fadec and avionic component distributed architecture

B - Operations, Transporting

64

D

B64D 31/00 (2006.01) B64D 43/00 (2006.01) F02C 9/00 (2006.01)

Patent

CA 2698106

The invention relates to a device for motorized aircraft comprising at least one avionic component (300) positioned in the said aircraft, at least one engine interface (310) positioned in the said aircraft and at least one engine controller (315) positioned in or near an engine (320) of the said aircraft. According to the device of the invention, the said at least one engine interface (310) is designed to exchange data between the said at least one avionic component (300) and the said at least one engine controller (315). The said at least one engine interface (310) is generic and able to communicate with engine controllers (315) of various types that may be mounted on said aircraft. The said at least one engine controller is specific to a particular engine.

L'invention concerne un dispositif pour aéronef motorisé comprenant au moins un composant avionique (300) positionné dans ledit aéronef, au moins une interface moteur (310) positionnée dans ledit aéronef et au moins un contrôleur moteur (315) positionné dans ou à proximité d'un moteur (320) dudit aéronef. Selon le dispositif de l'invention, ladite au moins une interface moteur (310) est adaptée à échanger des données entre ledit au moins un composant avionique (300) et ledit au moins un contrôleur moteur (315). Ladite au moins une interface moteur (320) est générique et adaptée à communiquer avec des contrôleurs moteur (315) de différents types pouvant être montés sur ledit aéronef. Ledit au moins un contrôleur moteur est spécifique à un moteur

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