发明名称 Method for joining single crystal turbine blade halves.
摘要 Single-crystal, nickel-based superalloy turbine blades (10) are formed by fusion-welding together two matched blade halves (12,14). The matched blade halves (12,14) are joined by an electrospark deposition process which deposits a weld filler metal along matched faying surfaces. The deposited weld filler metal is preferably the same nickel-based superalloy used to form the single-crystal turbine blades (10). Total heat input to the base metal is minimal so that distortion and metallurgical structure changes of the base metal are virtually non-existent. <IMAGE>
申请公布号 EP0503696(B1) 申请公布日期 1995.07.19
申请号 EP19920200493 申请日期 1992.02.20
申请人 GENERAL MOTORS CORPORATION 发明人 HEITMAN, PETER WARREN;BROWN, LAWRENCE EVANS;HAMMOND, STEPHEN NORMAN
分类号 B23K1/00;B23K11/10;B23K20/00;B23P15/04;F01D5/14;F01D5/18;F01D5/28;F01D5/30;(IPC1-7):F01D5/14;B23K11/087 主分类号 B23K1/00
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