| 发明名称 | Ceramic matrix composite airfoil structure with trailing edge support for a gas turbine engine | ||
| 摘要 | An airfoil for a gas turbine engine includes an aft trailing edge support between a pressure side and a suction side. | ||
| 申请公布号 | US8967961(B2) | 申请公布日期 | 2015.03.03 |
| 申请号 | US201113309514 | 申请日期 | 2011.12.01 |
| 申请人 | United Technologies Corporation | 发明人 | McCaffrey Michael G. |
| 分类号 | F01D5/14 | 主分类号 | F01D5/14 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. An airfoil for a gas turbine engine comprising: a pressure side formed of at least one Ceramic Matrix Composite ply; a suction side formed of at least one Ceramic Matrix Composite ply; andan aft trailing edge support between said pressure side and said suction side, wherein an open portion of said aft trailing edge support is open toward a trailing edge where said pressure side meets said suction side. | ||
| 地址 | Hartford CT US | ||