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 |
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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