초록 ▼

An aircraft propulsion system (10) is connected to a strut, fixed to the wing or fuselage, by a fixing device comprising at least one rear mount (22) and two front mounts (24, 26). The rear mount (22) and a first (24) of the front mounts connect a main part (12a) of the frame (12) of the strut to th

An aircraft propulsion system (10) is connected to a strut, fixed to the wing or fuselage, by a fixing device comprising at least one rear mount (22) and two front mounts (24, 26). The rear mount (22) and a first (24) of the front mounts connect a main part (12a) of the frame (12) of the strut to the central casing (16) of the engine. The other front mount (26) connects a front part (12b) projecting from the strut frame (12) to the fan stator case (20) and mainly takes up the vertical forces (Z). Thus, the first front mount (24) can be simplified and bending or sagging of the engine is reduced.

대표청구항 ▼

1. Device for fixing an aircraft propulsion system to a strut fixed to a structural element of the aircraft, the propulsion system including an engine having a central casing and a fan stator case, the device comprising:a first front mount and at least one rear mount, respectively directly connectin

1. Device for fixing an aircraft propulsion system to a strut fixed to a structural element of the aircraft, the propulsion system including an engine having a central casing and a fan stator case, the device comprising:a first front mount and at least one rear mount, respectively directly connecting to the strut a front part and a rear part of the central casing of the engine; and at least one second front mount directly connecting the fan stator case to the strut.