|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/226.2; 239/265.31; 244/110.B|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 14 인용 특허 : 59|
Aircraft systems having thrust reversers with support members are disclosed herein. In one embodiment, an aircraft system includes a thrust reverser having a nozzle inner wall, a nozzle outer wall radially outward of the inner wall, and a blocker door carried by the outer wall. The blocker door is movable between a deployed position and a stowed position. The thrust reverser further includes a support member extending between a forward section of a nozzle inner wall and a forward section of the nozzle outer wall. The support member is positioned such tha...
I claim: 1. An aircraft system, comprising a thrust reverser including: a nozzle inner wall; a nozzle outer wall radially outward of the nozzle inner wall, the nozzle outer wall including a blocker door movable between a deployed position and a stowed position; a fixed structure positioned radially outward of the nozzle outer wall; a link having a first end portion pivotally coupled to the fixed structure and a second end portion spaced apart from the first end portion; and a support member extending between the nozzle inner wall and the nozzle outer wa...