发明名称 |
Low-mid turbine temperature abradable coating |
摘要 |
In order to minimize a clearance between a turbine and its housing, and thus, improve the efficiency of a turbine engine, an abradable coating can be applied to an inner surface of the turbine housing. However, there are no known abradable coatings that can be applied to a housing that is subjected to temperatures between 950-1500° F. for extended periods of time. The apparatus of the present disclosure includes a housing including a 950-1500° F. section in which at least one rotating blade row is positioned. The rotating blades and the 950-1500° F. section each includes a surface being comprised of a relatively non-abradable material. The surface of the housing comprised of the relatively non-abradable material is covered by a 950-1500° F. relatively abradable coating that includes a metallic matrix and at least one of a thermoplastic and dry lubricant. The metallic matrix is 55-85% of the coating by volume.
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申请公布号 |
US2005281668(A1) |
申请公布日期 |
2005.12.22 |
申请号 |
US20040872609 |
申请日期 |
2004.06.21 |
申请人 |
NAVA IRENE L;COE MICHAEL A |
发明人 |
NAVA IRENE L.;COE MICHAEL A. |
分类号 |
C23C4/04;C23C30/00;F01D5/20;F01D11/12;(IPC1-7):F01D5/20 |
主分类号 |
C23C4/04 |
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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