| 发明名称 | In-situ turbine blade tip repair | ||
| 摘要 | The tip portion of a blade of a gas turbine is repaired in-situ in the gas turbine without removing the blade from the turbine rotor disk. To facilitate the in-situ repair of the tip portion of the turbine blades, one or more access holes may be provided in the turbine shroud or blade outer air seal circumscribing the plurality of turbine blades extending radially outward from the turbine rotor dick. | ||
| 申请公布号 | US9085053(B2) | 申请公布日期 | 2015.07.21 |
| 申请号 | US200912644396 | 申请日期 | 2009.12.22 |
| 申请人 | United Technologies Corporation | 发明人 | Tholen Susan M.;Lutjen Paul M. |
| 分类号 | F01D11/08;B23P6/00;F01D5/00 | 主分类号 | F01D11/08 |
| 代理机构 | Miller, Matthias & Hull LLP | 代理人 | Miller, Matthias & Hull LLP |
| 主权项 | 1. A method for repairing a tip portion of a turbine blade of a gas turbine having a turbine rotor disk having a plurality of turbine blades and a turbine shroud circumscribing the turbine rotor disk, the method comprising the step of: providing at least one access opening in the turbine shroud, the at least one access opening having an airfoil shape; rebuilding the tip portion of the rotor blade in-situ without removing the blade form the turbine rotor disk; and providing a removable seal plug, having the airfoil shape, in the at least one access opening in the turbine shroud. | ||
| 地址 | Hartford CT US | ||