Mounting system inserted between an aircraft engine and a...

Details Mounting system inserted between an aircraft engine and a... Mounting system inserted between an aircraft engine and a...

B - Operations, Transporting

64

D

B64D 27/18 (2006.01) B64D 27/26 (2006.01) F01D 25/28 (2006.01)

Patent

CA 2499378

This invention relates to a mounting system (1) inserted between an aircraft engine and a rigid structure of an attachment strut, the system particularly comprising a thrust resistance device (20). The thrust resistance device (20) comprises two lateral actuators (30) each provided with a rod (34) in which a forward end (34b) is a piston located inside a chamber (38) of a central casing (22) of the engine, the chamber (38) comprising a forward compartment (40) and an aft compartment (42). Moreover, the thrust resistance device (20) comprises a device (32) including a piston (48) fixed to the forward mount (16) and located inside a chamber (50) fixed to the central casing, the chamber (50) comprising a forward compartment (52) and an aft compartment (54), the forward compartment (52) of the chamber (50) being hydraulically connected to the aft compartments (42) of the actuators (30).

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