发明名称 |
Method for vibrational damping of gas turbine engine airfoils |
摘要 |
A coating system and coating method for damping vibration in an airfoil of a rotating component of a turbomachine. The coating system includes a metallic coating on a surface of the airfoil, and a ceramic coating overlying the metallic coating. The metallic coating contains metallic particles dispersed in a matrix having a metallic and/or intermetallic composition. The metallic particles are more ductile than the matrix, and have a composition containing silver and optionally tin. The method involves ion plasma cleaning the surface of the airfoil before depositing the metallic coating and then the ceramic coating.
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申请公布号 |
US8017195(B2) |
申请公布日期 |
2011.09.13 |
申请号 |
US20070748625 |
申请日期 |
2007.05.15 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
DAROLIA RAMGOPAL;WEAVER MATTHEW MARK;CORBLY DENNIS MARTIN;MOVCHAN BORIS ALEXEEVICH;USTINOV ANATOLII IVANOVICH |
分类号 |
B05D3/00;C23C4/00;C23C4/02;C23C4/06;C23C14/02;C23C14/14;C23C30/00 |
主分类号 |
B05D3/00 |
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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