AIRCRAFT ENGINE UNIT

摘要

The invention relates to an aircraft engine unit (1) comprising a jet engine (2), a suspension pylon (4) and a plurality of engine fasteners. According to said invention, the plurality of fasteners comprises first (6a) and second (6b) front fasteners which are fixed to the fan case of the engine and positioned symmetrically with respect to a plane (P) defined by a longitudinal axis (5) of the jet engine and a vertical direction (Z) thereof, wherein the first and second fasteners are constructed in such a way that they pick up loads produced in the longitudinal direction (X) of the jet engine and in the vertical direction thereof. In addition, the plurality of fasteners also comprises a rear engine fastener (9) constructed in such a way that it picks up loads produced in the vertical direction.