|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-033/02 B64D-027/18 B64D-027/24 B64D-027/26 F01D-015/10 F02C-007/32 F02K-003/062 F04D-029/32 F04D-029/36 F04D-029/52 F04D-029/54 B64C-001/16 B64C-021/06 B64D-027/20 B64D-029/04 B64D-027/02|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 38|
A propulsion system for an aircraft is provided having an aft engine configured to be mounted to the aircraft at an aft end of the aircraft. The aft engine includes a fan rotatable about a central axis of the aft engine having a plurality of fan blades attached to a fan shaft. The aft engine also includes a nacelle encircling the plurality of fan blades and a structural support system for mounting the aft engine to the aircraft. The structural support system extends from the fuselage of the aircraft, through the fan shaft, and to the nacelle when the aft...
1. A propulsion system for an aircraft having a fuselage, the propulsion system comprising: an aft engine configured to be mounted to the aircraft at an aft end of the aircraft, the aft engine defining a central axis and comprising: a fan rotatable about the central axis of the aft engine and including a plurality of fan blades attached to a fan shaft;a nacelle encircling the plurality of fan blades of the fan and extending around a mean line of the aircraft at the aft end of the aircraft when the aft engine is mounted to the aircraft; anda structural su...