|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-003/06 F02K-001/20 F02C-003/06 F02C-007/20|
|미국특허분류(USC)||60/226R ; 60/226A ; 60/3931 ; 244/54|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 30 인용 특허 : 1|
A nacelle for use with a gas turbine engine is provided with an integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine. The nacelle is entirely supported in its spacial relationship with the engine by means of the webbed structure. The inner surface of the nacelle defines the outer limits of the engine motive fluid flow annulus while the outer surface of the nacelle defines a streamlined envelope for the engine.
A gas turbofan engine including a fan bypass flow annulus having an inlet and an exit, a core engine having an inlet duct communicating with said annulus, and a nacelle comprising: pairs of axially spaced outer, intermediate and inner coannular composite hoops, web means of composite filament construction rigidly bonding the axially forwardmost of each of said pairs of hoops together and further bonding the axially rearwardmost of each of said pairs of hoops together, wherein said pair of inner hoops is disposed within and attached to said core engine ra...