发明名称 |
Run-in coating for axial-flow compressor of gas turbine engines and method of using and making same |
摘要 |
Metal wire bundles are combined into brushes as a run-in coating for the axial-flow compressor stage of a gas turbine engine. The metal wire bundles are inserted into the basic material or are combined into brush segments that are inserted into corresponding recesses of the rotor housing.
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申请公布号 |
US6910856(B2) |
申请公布日期 |
2005.06.28 |
申请号 |
US20030667130 |
申请日期 |
2003.09.22 |
申请人 |
MTU AERO ENGINES GMBH |
发明人 |
RUELKE KAI |
分类号 |
F01D11/12;F04D29/16;(IPC1-7):F01D11/12 |
主分类号 |
F01D11/12 |
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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