发明名称 HIGH-STRENGTH SUPERALLOY JOINING METHOD FOR REPAIRING TURBINE BLADES
摘要 A method of repairing high-strength superalloy turbine blades and joining superalloy components is provided. A damaged region of the turbine blade is welded without preheating it. The welded turbine blade is then subjected to a hot isostatic pressing process. The method results in a repaired turbine blade that has a desirable microstructure and robust mechanical properties.
申请公布号 EP1697081(A1) 申请公布日期 2006.09.06
申请号 EP20040822140 申请日期 2004.12.06
申请人 HONEYWELL INTERNATIONAL INC. 发明人 HU, YIPING
分类号 B23K20/02;B23K15/00;B23K26/00;B23K26/32;B23K26/34;B23P6/00;B23P6/04;F01D5/00 主分类号 B23K20/02
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