Engine assembly for aircraft, has front and rear engine mounts placed between engine and strut, where front engine mounts are fixed to fan casing and designed to recover force exerted along longitudinal and vertical directions of engine

摘要

The assembly has front and rear engine mounts (6a, 6b, 8, 9) placed between a turbojet engine (2) and a hooking strut (4). The front engine mounts (6a, 6b) are fixed to a fan casing (12) of the engine and symmetrically located with respect to a plane defined by a longitudinal axis (5) and a vertical direction of the engine, where each front engine mount is designed to recover a force exerted along longitudinal and vertical directions of the engine. The mount (9) recovers the force exerted along the vertical direction of the engine. An independent claim is also included for an aircraft comprising an engine assembly.