发明名称 |
Method for coating gas turbine engine components |
摘要 |
A method for assembling a vane sector for a gas turbine engine, the vane sector including an airfoil vane and a platform includes depositing a wear coating material onto a selected area of the platform, positioning the platform adjacent to the airfoil vane, and executing a brazing operation such that the airfoil vane is permanently coupled to the platform portion and such that the wear coating material is bonded across a predefined area of the platform.
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申请公布号 |
US7331755(B2) |
申请公布日期 |
2008.02.19 |
申请号 |
US20040853609 |
申请日期 |
2004.05.25 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BRODERICK THOMAS FROATS;GALLEY RONALD LANCE;SHAMBLEN CLIFFORD EARL;BUDINGER DAVID EDWIN;OLIVER REED ROY;BARBE ROGER OWEN |
分类号 |
F01D9/00;B05D3/00;B05D7/00;B23K1/00;B23P15/04;C23C28/00;F01D5/08;F01D5/14;F01D5/28;F01D9/04;F01D11/12;F02C7/00 |
主分类号 |
F01D9/00 |
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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