|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/110B; 244/131; 060/226.2|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 20 인용 특허 : 190|
A pivot arrangement for a thrust reverser door of a gas turbine engine, the pivot fitting having a base and a shaft projecting from a main side of the base. The shaft receives a preferably curved pivot arm of the door to provide a low profile arrangement which improves performance when the doors are stowed.
1. A thrust reverser comprising: first and second doors, each having a pair of opposed pivot arms;a jet pipe having a pair of jet pipe arms and a radially inner mold line surface for bounding discharge of exhaust gas; anda pair of pivot fittings inserted into corresponding recesses radially inside each jet pipe arm substantially flush with said inner mold line surface, each pivot fitting having a projection extending outwardly through an opening in the jet pipe arm, each projection received in a pivot hole in a corresponding pivot arm. 2. A thrust revers...