| 发明名称 | Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine | ||
| 摘要 | A vane structure for a gas turbine engine includes a multiple of CMC airfoil sections integrated between a CMC outer ring and a metal alloy inner ring. | ||
| 申请公布号 | US8770931(B2) | 申请公布日期 | 2014.07.08 |
| 申请号 | US201113116144 | 申请日期 | 2011.05.26 |
| 申请人 | United Technologies Corporation | 发明人 | Alvanos Ioannis;Suciu Gabriel L. |
| 分类号 | F01D9/04;F01D25/24 | 主分类号 | F01D9/04 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. A vane structure for a gas turbine engine comprising: a CMC outer ring; a metal alloy inner ring; and a multiple of CMC airfoil sections between said CMC outer ring and said metal alloy inner ring. | ||
| 地址 | Hartford CT US | ||