发明名称 |
Retarding and filter cleaning method and system |
摘要 |
A filter cleaning system is provided for a gas turbine engine including a compressor section and a combustor section. A mechanism is operatively connected to the gas turbine engine and is configured to be driven by the gas turbine engine in a first mode and configured to drive the gas turbine engine in a second mode. A first flow path is for delivering compressed air to the compressor section. At least one air filter is configured to filter air entering the first flow path. A second flow path is for delivering compressed air from the compressor section to the combustor section in the first mode. A third flow path is for delivering compressed air from the compressor section to the at least one air filter during the second mode.
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申请公布号 |
US2007119146(A1) |
申请公布日期 |
2007.05.31 |
申请号 |
US20050289321 |
申请日期 |
2005.11.30 |
申请人 |
CATERPILLAR INC. |
发明人 |
CALLAS JAMES J.;MARTIN KEVIN L.;RENSHAW CODY P.;SOPKO THOMAS M.;TONSOR ANDREW J. |
分类号 |
F02C7/052 |
主分类号 |
F02C7/052 |
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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