|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/20 F02K-003/06 F02K-003/00|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 29 인용 특허 : 13|
A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.
We claim: 1. A casing for an aircraft turbofan bypass engine, the casing comprising: a case adapted to encircle the engine and having a plurality of engine mounts thereon adapted to mount the engine to an aircraft; an inner hub adapted to support at least one bearing supporting a main shaft of the engine, the inner hub supported inside the case by a plurality of struts extending between the inner hub to the case, the struts defining a primary load path from the inner hub to the case; and a splitter supported intermediate the inner hub and case by the st...