B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01) B64D 27/18 (2006.01)
Patent
CA 2657397
The invention relates to an engine assembly for an aircraft, comprising an engine, an engine mounting device (4) and a cowling enclosing the engine provided with fan shrouds (34), the mounting device (4) having a rigid structure (8) and a forward aerodynamic structure (24) on which the fan shrouds have an articulated mounting, said forward aerodynamic structure (24) being provided with a cradle (40) having rear mounting means (44a, 44b) fixed to the rigid structure (8). According to the invention, the cradle is also provided with forward mounting means (42) fixed to an engine fan housing (18).
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 un carter de soufflante (18) du moteur.
Martinou Jean-Marc
Roche Frederic
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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