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
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