|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F01D-017/14 F02C-007/042 B64D-029/00 B64D-029/06 B64D-033/02|
|우선권정보||DE-10 2011 103 163 (2011-06-01)|
|§371/§102 date||20140114 (20140114)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 5|
An aircraft gas-turbine engine has an engine cowling-nacelle which surrounds a core engine in a tubular way, characterized in that at least one inflow-side part of the engine cowling-nacelle is telescopically movable against the flow direction.
1. An aircraft gas-turbine engine comprising: a core engine including a core engine casing,an engine cowling spaced radially outwardly of the core engine casing and surrounding the core engine casing in a tubular manner forming a bypass duct, the engine cowling including an outer portion, an inner portion and an inflow-side part,a fan connected to the core engine,a bypass fan casing surrounding the fan and forming a portion of the bypass duct,wherein the inflow-side part is tubular, extends around an entire circumference of the engine cowling, and is tel...