发明名称 |
GAS TURBINE ENGINE AND INTEGRATED HEAT EXCHANGE SYSTEM |
摘要 |
One embodiment of a heat exchange system is disclosed having a heat exchange compressor and multiple evaporators capable of operating at different heat transfer requirements. The heat exchange compressor may be a single-stage or multi-stage compressor. In one form the evaporators return working fluid in separate streams to the heat exchange compressor. The heat exchange compressor may be integrated with a gas turbine engine and includes a number of inlets that correspond to a number of separate evaporators. Each inlet can be configured to receive working fluid at different locations within a pressure and velocity flow field created in the compressor. The heat exchange compressor may be driven by a shaft of the gas turbine engine and may be positioned at a variety of locations. |
申请公布号 |
EP2310652(A4) |
申请公布日期 |
2013.08.14 |
申请号 |
EP20090767109 |
申请日期 |
2009.06.19 |
申请人 |
ROLLS-ROYCE CORPORATION |
发明人 |
JUNOD, LARRY, ALLEN |
分类号 |
F02C1/00;F01D15/00;F01D15/08;F02C7/141;F02G3/00 |
主分类号 |
F02C1/00 |
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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