发明名称 TURBINE ENGINE WITH AIR COOLED TURBINE
摘要 In a turbine engine (10), low temperature air is diverted from a low pressure section of the compressor section of the engine to cool the high pressure turbine of the engine. Low pressure air is diverted from the compressor section, and its pressure is thereafter be increased. the pressure is increased in an intermediate cavity (80) in the engine, where rotational energy of the diverted air is converted to static pressure by way of an obstruction (88) that converts dynamic head of the air in the cavity into static pressure.
申请公布号 WO03038254(A1) 申请公布日期 2003.05.08
申请号 WO2002CA01574 申请日期 2002.10.18
申请人 PRATT & WHITNEY CANADA CORP. 发明人 LIU, XIAOLIU
分类号 F02C1/00;F01D5/08;F01D9/06;F01D25/12;F02C7/12;F02C7/18;(IPC1-7):F02C7/18 主分类号 F02C1/00
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