Aircraft engine assembly

Details Aircraft engine assembly Aircraft engine assembly

B - Operations, Transporting

64

D

B64D 27/26 (2006.01)

Patent

CA 2624017

The invention relates to an engine assembly for an aircraft, consisting of a turbojet, a pylon and a plurality of engine mounts, the latter comprising first and second front mounts (6a) which are fixed to the fan case and which are disposed symmetrically in relation to a plane defined that is by a longitudinal axis of the turbojet and a vertical direction of same, said two front mounts each having been designed to pick up loads exerted in a longitudinal direction of the turbojet and in the vertical direction of same. In addition, each of the two front mounts comprises a shear slug (36) which is mounted to the case (12) and which extends through the two sides (32a, 32b) of a clevis (30) that is fixed to the pylon.

L'invention se rapporte à un ensemble moteur pour aéronef comprenant un turboréacteur, un mât d'accrochage ainsi qu'une pluralité d'attaches moteur. Cette dernière comprend une première et une seconde attache avant (6a) fixées au carter de soufflante et situées de façon symétrique par rapport à un plan défini par un axe longitudinal du turboréacteur et une direction verticale de celui-ci, les deux attaches avant étant chacune conçues de manière à reprendre des efforts s'exerçant selon une direction longitudinale du turboréacteur et selon la direction verticale de celui- ci. De plus, chacune des deux attaches avant comporte un pion de cisaillement (36) monté sur le carter (12) et traversant les deux flancs (32a, 32b) d'une chape (30) montée fixement sur le mât.

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