|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 10 인용 특허 : 50|
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 bypass turbofan 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 relative to the case by a plurality of struts extending between the inner hub to the case, the inner hub having a semi-monocoque configuration including a plurality of stiffeners and a plurality of thin-walled shear panels there...