| 发明名称 |
Method for manufacturing a turbine engine component |
| 摘要 |
A layered structure (26) comprises a base structure (28) having a major surface (32, 34), and a brazing layer (30a, 30b) secured to the major surface (32, 34) of the base structure (28), where the brazing layer (30a, 30b) is applied to the major surface (32, 34) prior to positioning the layered structure in contact with a turbine engine component. |
| 申请公布号 |
EP1987903(A2) |
申请公布日期 |
2008.11.05 |
| 申请号 |
EP20080251540 |
申请日期 |
2008.04.28 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BISCHOF, CHRISTOPHER J.;MINOR, MICHAEL J.;PELLET, PAUL M.;HUXOL, JASON E. |
| 分类号 |
B23K1/00;B23K1/20;B23K101/00;B23K103/08;B23P15/02;F01D5/30 |
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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