发明名称 |
Gas turbine engine air cycle system |
摘要 |
An air cycle system (100) for a gas turbine engine includes a compressor (62), a turbine (64) and a heat exchanger (66) fluidly connected between the compressor (62) and the turbine (64). A fluid source (92) communicates a fluid through the heat exchanger (66). The heat exchanger (66) exchanges heat between the fluid and an airflow communicated through the heat exchanger (66) from the compressor (62) to provide a conditioned airflow. |
申请公布号 |
EP2565392(A2) |
申请公布日期 |
2013.03.06 |
申请号 |
EP20120182560 |
申请日期 |
2012.08.31 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
FINNEY, ADAM;ANDRES, MICHAEL |
分类号 |
F01D25/12;F02C3/36 |
主分类号 |
F01D25/12 |
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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