ENGINE ASSEMBLY FOR AIRCRAFT

摘要

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.