| 发明名称 | Airfoil seal | ||
| 摘要 | A gas turbine engine component has an airfoil and a squealer tip. The airfoil has a pressure side and a suction side. The squealer tip is located at one end of the airfoil to engage with an adjacent surface and thereby form a seal. The squealer tip terminates in a squealer tip apex with an arched cross-sectional profile in a plane extending from the pressure side to the suction side of the airfoil. A method for producing an airfoil seal for the gas turbine engine component is also provided. | ||
| 申请公布号 | US8858167(B2) | 申请公布日期 | 2014.10.14 |
| 申请号 | US201113212709 | 申请日期 | 2011.08.18 |
| 申请人 | United Technologies Corporation | 发明人 | Baumann Paul W. |
| 分类号 | F01D5/20;F01D11/08;F01D5/14;F01D11/00 | 主分类号 | F01D5/20 |
| 代理机构 | Kinney & Lange, P.A. | 代理人 | Kinney & Lange, P.A. |
| 主权项 | 1. A gas turbine engine component comprising: an airfoil having a pressure side and a suction side; and a metallic squealer tip located at one end of the airfoil to engage with an adjacent surface and thereby form a seal, the squealer tip terminating in a squealer tip apex that follows a continuously curved circular or elliptical cross-sectional profile in a plane extending from the pressure side to the suction side of the airfoil. | ||
| 地址 | Hartford CT US | ||