发明名称 |
Method of coating gas turbine components |
摘要 |
A method of forming a metal coating on surfaces of internal passages of a turbine part (40) includes applying a nickel aluminum bond coating to an external surface of the turbine part, positioning the turbine part in a VPA chamber (88), coupling a gas manifold to at least one internal passage inlet, and coating at least a portion of the internal surface and the external of the turbine part by a vapor phase aluminiding (VPA) process using metal coating gases to form a coating on the internal surfaces of the turbine part.
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申请公布号 |
EP1820876(A1) |
申请公布日期 |
2007.08.22 |
申请号 |
EP20070101752 |
申请日期 |
2007.02.05 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
GUPTA, BHUPENDRA KUMAR;DAS, NRIPENDRA NATH;SAYLOR, MATTHEW DAVID;ZIMMERMAN, ROBERT GEORGE, JR. |
分类号 |
C23C10/06;C23C10/14;C23C28/00;C23C30/00 |
主分类号 |
C23C10/06 |
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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