|국가/구분||United States(US) Patent 등록|
|우선권정보||FR-06 52912 (2006-07-11)|
|§371/§102 date||20081231 (20081231)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 16 인용 특허 : 8|
An aircraft engine assembly including an engine, an engine mounting structure, and a nacelle surrounding the engine and including an air intake and fan cowls. The assembly further includes a cradle supporting the fan cowls, fixedly mounted on the mounting structure or else on an entity including a fan case and the air intake attached to the case. The engine assembly further includes a junction aerodynamic fairing including a first mounting mechanism mounted on the cradle, and including a second mounting mechanism mounted on the other of the elements from...
1. An aircraft engine assembly comprising: an engine;an engine mounting structure;a nacelle surrounding the engine and comprising an air intake and fan cowls;a cradle on which the fan cowls are movably mounted, the cradle being fixedly mounted on one of the engine mounting structure and a fan assembly comprising a fan case for the engine and the air intake attached to the fan case;a cradle aerodynamic cowling housing said cradle, anda junction aerodynamic fairing extending longitudinally with said cradle aerodynamic cowling along a longitudinal axis X of...