发明名称 |
GAS TURBINE ENGINE BUFFER COOLING SYSTEM |
摘要 |
A gas turbine engine includes a heat exchanger, a mid-turbine frame, a passageway that extends through at least a portion of the mid-turbine frame and a first nozzle assembly. The heat exchanger exchanges heat with a bleed airflow to provide a conditioned airflow. The mid-turbine frame is in fluid communication with the heat exchanger. The conditioned airflow is communicated through the passageway and is received by the first nozzle assembly to condition gas turbine engine hardware. |
申请公布号 |
WO2013130307(A1) |
申请公布日期 |
2013.09.06 |
申请号 |
WO2013US26766 |
申请日期 |
2013.02.20 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU, GABRIEL L.;ALVANOS, IOANNIS |
分类号 |
F02C7/12;F01D9/02;F01D25/12 |
主分类号 |
F02C7/12 |
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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