| 发明名称 | Spoked spacer for a gas turbine engine | ||
| 摘要 | A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation and a plurality of core gas path seals which extend from the rotor ring, each of the plurality of core gas path seals extend from the rotor ring at an interface, the interface defined along a spoke. | ||
| 申请公布号 | US8944762(B2) | 申请公布日期 | 2015.02.03 |
| 申请号 | US201113283733 | 申请日期 | 2011.10.28 |
| 申请人 | United Technologies Corporation | 发明人 | Suciu Gabriel L.;Muron Stephen P.;Dye Christopher M. |
| 分类号 | F01D5/06;F01D11/00 | 主分类号 | F01D5/06 |
| 代理机构 | Carlson, Gaskey & Olds, PC | 代理人 | Carlson, Gaskey & Olds, PC |
| 主权项 | 1. A spacer for a gas turbine engine comprising: a rotor ring defined along an axis of rotation; and a plurality of core gas path seals which extend from said rotor ring, each of said plurality of core gas path seals extend from said rotor ring at an interface, said interface defined along a spoke, and wherein said interface includes a heat treat transition. | ||
| 地址 | Hartford CT US | ||