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. |
申请公布号 |
GB2414430(B) |
申请公布日期 |
2006.11.15 |
申请号 |
GB20050009617 |
申请日期 |
2005.05.11 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
THOMAS FROATS BRODERICK;RONALD LANCE GALLEY;CLIFFORD EARL SHAMBLEN;DAVID EDWIN BUDINGER;REED ROY OLIVER;ROGER OWEN BARBE |
分类号 |
C23C28/00;B05D3/00;B05D7/00;B23K1/00;F01D5/08;F01D5/14;F01D5/28;F01D9/04;F01D11/12;F02C7/00 |
主分类号 |
C23C28/00 |
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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