Airbus France

Guillaume Seguin

Lionel Diochon

Isabelle Petrissans

An engine assembly for aircraft including a turboshaft engine, an attachment strut, and a plurality of engine mounts interposed between the attachment strut and the turboshaft engine. The plurality of engine mounts include two forward mounts arranged in a staggered manner in relation to each other in a vertical direction of the turboshaft engine, the first forward mount configured to assure uniquely taking up of stresses brought to bear along the transversal direction of the turboshaft engine, and the second forward mount configured to assure uniquely taking up of stresses brought to bear along the transversal and vertical directions.

Engine assembly for aircraft

The invention relates to an engine assembly for an aircraft comprising a turbojet, a engine mount pylon, and a plurality of engine mounts inserted between the engine mount pylon and the turbojet. According to the invention, the plurality of engine mounts comprises a engine mount () designed so as to uniquely resist forces applied along a direction (Y) transverse to the turbojet, this engine mount () comprising an intermediate fitting () assembled onto a first fitting () fixed to the pylon through two swivel axes () oriented parallel along a vertical direction (Z), and a pin () oriented along a longitudinal direction (X) and fixed to the intermediate fitting, the pin being installed on a second fitting () fixed to the turbojet, with clearance along the longitudinal direction (X).

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Le Havre, France

Guillaume Seguin