|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 36|
A cam-type apparatus is included in a support link between outer and inner cases of gas turbine engines for centering the cases one to another. The cam-type apparatus is lockable to allow locking an adjusted position of the cam-type apparatus.
1. A turbofan gas turbine engine comprising: a core portion of the engine;an annular bypass duct wall coaxially surrounding and supporting the core portion, thereby to define an annular bypass air passage radially between the core portion and the bypass duct wall for directing a bypass air flow passing therethrough; anda support link having a plurality of rods extending across the annular bypass air passage to interconnect the core portion and the annular bypass duct wall, the plurality of rods being connected to the core portion by a cam-type apparatus,...