|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F01D-025/00 F01D-009/04 F01D-021/04|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 16|
A catcher for a gas turbine engine includes a central hub, a plurality of struts, and a first ring. The plurality of struts are connected to and extend outward from the central hub. The first ring is connected to a mid-section of the plurality of struts and extends therebetween.
1. A gas turbine engine comprising: a compressor impeller;a turbine wheel connected to the compressor impeller, wherein the turbine wheel has a center section with a first radial extent at a forward end and second radial extent at an aft end, the second radial extent being less than the first radial extent; andan exhaust housing positioned adjacent an outer perimeter of the turbine wheel, wherein the exhaust housing forms an outer boundary for a flow path directly aft of the turbine wheel;a catcher positioned axially aft of and spaced at a distance from ...