发明名称 |
GAS TURBINE ENGINE HEAT EXCHANGER |
摘要 |
A gas turbine engine having a heat exchanger is disclosed. In one form the gas turbine engine includes a particle separator that can be used to separate particles or foreign objects and create a dirty flow and a clean flow. A blower can be used to discharge the particles or foreign objects from the separator. The heat exchanger includes a relatively warm flow path from a downstream region of a compressor and a relatively cool flow path from an upstream region of the compressor. The relatively cool flow path is merged with the dirty flow. In another embodiment, the gas turbine engine is a turbofan and the relatively cool flow path is merged with a bypass flow. In one embodiment of the engine the relatively warm flow path, after having exchanged heat with the relatively cool flow path is delivered to a working component without passing through a turbomachinery component. |
申请公布号 |
US2012159961(A1) |
申请公布日期 |
2012.06.28 |
申请号 |
US201113336378 |
申请日期 |
2011.12.23 |
申请人 |
KRAUTHEIM MICHAEL STEPHEN;SOTO-GONZALEZ CARLOS |
发明人 |
KRAUTHEIM MICHAEL STEPHEN;SOTO-GONZALEZ CARLOS |
分类号 |
F02C6/08;F01N13/08 |
主分类号 |
F02C6/08 |
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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