| 发明名称 | Turbine hub retainer | ||
| 摘要 | A retainer for a gas turbine engine includes a center body, a plurality of struts, and a ring. The plurality of struts are connected to and extend outward from the center body. The ring is connected to the plurality of struts and is positioned aft of the center body with respect to a direction of airflow through the gas turbine engine. | ||
| 申请公布号 | US9540949(B2) | 申请公布日期 | 2017.01.10 |
| 申请号 | US201213713513 | 申请日期 | 2012.12.13 |
| 申请人 | Hamilton Sundstrand Corporation | 发明人 | Jewess Gordon F.;Sirinivasan Navindaran;Michalik Marek;McLaughlin James J.;Napier James C.;Kowiel Krzysztof;Miaskiewicz Agata |
| 分类号 | F01D25/16;F01D25/04;F02K1/04 | 主分类号 | F01D25/16 |
| 代理机构 | Kinney & Lange, P.A. | 代理人 | Kinney & Lange, P.A. |
| 主权项 | 1. A retainer for a gas turbine engine comprising: a center body; a plurality of struts connected to and extending outward from the center body in a downstream direction such that each strut forms an acute angle with a centerline axis of the gas turbine engine; and a ring connected to the plurality of struts, wherein the ring is positioned aft of the center body with respect to a direction of airflow through the gas turbine engine, wherein the ring is connected to and forms a portion of an exhaust housing of the gas turbine engine. | ||
| 地址 | Windsor Locks CT US | ||