B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01)
Patent
CA 2623760
The invention concerns an engine assembly (1) for an aircraft comprising an engine (6) and a device for locking (4) the engine, the locking device being designed to be interposed between a wing system of the aircraft and the engine, and comprising a rigid structure (8) as well as means for locking the engine (6) on said rigid structure, the locking means consisting of a first fastener (10) as well as a second fastener (12). The invention is characterized in that the first fastener comprises two lateral half- fasteners (10a) each fixed on a fan casing (18) of the engine, and the second fastener is fixed on a front part of a central casing (22) of said engine.
L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un moteur (6) et un dispositif d'accrochage (4) du moteur, le dispositif d'accrochage étant destiné à être interposé entre une voilure de l'aéronef et le moteur, et comportant une structure rigide (8) ainsi que des moyens d'accrochage du moteur (6) sur ladite structure rigide, les moyens d'accrochage étant constitués d'une première attache (10) ainsi que d'une seconde attache (12). Selon l'invention, la première attache comporte deux demi- attaches latérales (10a) chacune fixée sur un carter de soufflante (18) du moteur, et la seconde attache est fixée sur une partie avant d'un carter central (22) de ce moteur.
Diochon Lionel
Mastroberti Raffaella
Petrissans Isabelle
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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