|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||415/213.1; 248/554; 248/555; 060/226.1; 060/796|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 34|
A gas turbine engine has a rear mounting assembly incorporating a mounting apparatus attached to a bypass duct wall with a link device for transferring core portion related inertia-induced loads, from an MTF of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.
1. A turbofan gas turbine engine comprising: a front mounting assembly attached to an annular bypass duct wall at a front axial position close to an inlet of a bypass air passage defined radially between the bypass duct wall and a core portion of the engine, the core portion being supported within the bypass duct wall by the front mounting assembly;a rear mounting assembly having a mounting apparatus affixed to the bypass duct wall at a rear axial position adjacent to an outlet of the bypass air passage, the rear mounting assembly including a plurality o...