B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/18 (2006.01) B64D 27/26 (2006.01)
Patent
CA 2697380
The invention relates to an engine assembly for an aircraft, that comprises an engine, a device for attaching the engine (4) and a nacelle surrounding the engine and provided with fan coils (34) the attachment device (4) including a rigid structure (8) as well as a front aerodynamic structure (24) on which the fan coils are hinged, said front aerodynamic structure being equipped with a cradle (40) provided with rear attachment means (44a, 44b) mounted on the rigid structure (8). According to the invention, the cradle is also equipped with front attachment means (42) mounted on an air intake (32) of the nacelle.
La présente invention se rapporte à un ensemble moteur pour aéronef comprenant un moteur, un dispositif d'accrochage du moteur (4) ainsi qu'une nacelle entourant le moteur et pourvue de capots de soufflante (34), le dispositif d'accrochage (4) comportant une structure rigide (8) ainsi qu'une structure aérodynamique avant (24) sur laquelle les capots de soufflante sont articulés, cette structure aérodynamique avant (24) étant équipée d'un berceau (40) pourvu de moyens d'accrochage arrière (44a, 44b) montés sur la structure rigide (8). Selon l'invention, le berceau est également équipé de moyens d' accrochage avant (42) montés sur une entrée d'air (32) de la nacelle.
Dussol Loic
Ridray Frederic
Airbus Operations
Goudreau Gage Dubuc
LandOfFree
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