| 发明名称 |
METHOD FOR RECONTOURING A COMPRESSOR OR TURBINE BLADE OR VANE FOR A GAS TURBINE |
| 摘要 |
A method for recontouring a blade of a gas turbine includes systematically melting a portion of a leading edge of the blade using an energy beam so as to form a new contour of hardened material substantially without incorporating additional material. |
| 申请公布号 |
EP2611567(A1) |
申请公布日期 |
2013.07.10 |
| 申请号 |
EP20110749091 |
申请日期 |
2011.08.22 |
| 申请人 |
LUFTHANSA TECHNIK AG |
发明人 |
CZERNER, STEFAN |
| 分类号 |
B23K26/00;B23K101/00;B23K101/14;B23K101/34;B23K103/00;B23K103/14;B23K103/18;B23P6/00;F01D5/00 |
主分类号 |
B23K26/00 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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