发明名称 |
TURBINE BLADE REPAIR METHOD |
摘要 |
PURPOSE: A turbine blade repairing method is provided to lower welding defect generation sensitivity by releasing the hardening property of a heat affected zone and to improve mechanical property by applying a weld bead lamination process. CONSTITUTION: A turbine blade repairing method comprises following steps. Filler materials of which mechanical property is strengthened are selected. A damaged part of a turbine blade is partially heated to be repaired. A multi-layered laminate repair welding process is enabled on a heated damaged part using a heat input adjustment step(S126) and a starting position adjusting step(S127) of weld bead. After the repair welding process, direct post heat temperature is maintained, and a welding-post thermal process is enabled. |
申请公布号 |
KR20100069084(A) |
申请公布日期 |
2010.06.24 |
申请号 |
KR20080127660 |
申请日期 |
2008.12.16 |
申请人 |
DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD. |
发明人 |
SONG, KEUN HO;KIM, IN SOO |
分类号 |
F01D5/12;F01D25/00 |
主分类号 |
F01D5/12 |
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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