发明名称 METHOD AND SYSTEM FOR IMPROVING EFFICIENCY OF MULTISTAGE TURBOCHARGER
摘要 A turbine system for a multistage turbocharger and a method for utilizing the same are disclosed. The turbine system includes a high pressure turbine having an inlet for receiving a flow of fluid, and an outlet for passing the flow on extraction of work from the high pressure turbine. The system further includes a low pressure turbine, having an inlet for receiving a flow of fluid from the high pressure turbine. A diffuser connects the outlet of the high pressure turbine and the inlet of the low pressure turbine. The system also includes a bypass channel for bypassing a portion of the flow around the high pressure turbine, from upstream of the high pressure turbine to downstream of the high pressure turbine. The system includes an injector to input the bypass flow in the diffuser in a manner to reduce flow separation in the diffuser.
申请公布号 US2012227400(A1) 申请公布日期 2012.09.13
申请号 US201113043826 申请日期 2011.03.09
申请人 ERDMENGER RODRIGO RODRIGUEZ;GRECO ALBERTO SCOTTI DEL;MICHELASSI VITTORIO;SWENSON KENDALL ROGER;LORINGER DANIEL EDWARD;STABLEIN MARK THOMAS;JOHNSON LUKAS WILLIAM;GENERAL ELECTRIC COMPANY 发明人 ERDMENGER RODRIGO RODRIGUEZ;GRECO ALBERTO SCOTTI DEL;MICHELASSI VITTORIO;SWENSON KENDALL ROGER;LORINGER DANIEL EDWARD;STABLEIN MARK THOMAS;JOHNSON LUKAS WILLIAM
分类号 F02C6/12 主分类号 F02C6/12
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