|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/054; 060/796; 060/797; 248/554; 248/556; 248/557; 248/555|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 19 인용 특허 : 11|
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 (3...
The invention claimed is: 1. Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft, the system including a forward mount, an aft mount, and a device for resisting thrusts generated by the engine, wherein: said device comprises two lateral actuators arranged one on each side of the engine, each actuator being provided with a rod in which an aft end is connected to one of said forward and aft mounts and for which one forward end is a piston located inside a chamber fixed to a f...