发明名称 GAS TURBINE EJECTOR AND METHOD OF OPERATING THE SAME
摘要 PROBLEM TO BE SOLVED: To provide a system improving a cooling performance of a turbine engine by utilizing an ejector system that improves an air entrainment efficiency of a compressor. SOLUTION: An ejector system (34) for combining a high-pressure and low-pressure fluid flow streams (18) and a method of operating the same are disclosed. A nozzle chamber (35) communicates with the high-pressure fluid flow stream, and a suction chamber (42) communicates with the low-pressure fluid flow stream (18). An exit (40) of the nozzle chamber (35) exits from the suction chamber (42), and includes a plurality of nozzles (48) so that the high-pressure fluid flow stream exits from the nozzle chamber (35) by a plurality of flow streams having a plurality of surface sections against an interlayer drag between the streams. The low-pressure fluid flow stream (18) is entrained by the high-pressure fluid flow streams flowing out from the plurality of nozzles (48) to form a middle-pressure flow stream. COPYRIGHT: (C)2010,JPO&INPIT
申请公布号 JP2010101315(A) 申请公布日期 2010.05.06
申请号 JP20090235838 申请日期 2009.10.13
申请人 GENERAL ELECTRIC CO <GE> 发明人 ZHANG HUA;BALL JR DAVID WESLEY;ELURIPATI RAVI PRAVEEN;POMPEY CHRISTINA RENEE;WHALING KENNETH NEIL
分类号 F02C7/18;F04F5/20;F04F5/46 主分类号 F02C7/18
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