发明名称 An inlet system for a gas turbine with EGR system
摘要 An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine (140) where it may be mixed with the inlet air and re-enter the turbomachine (140) without affecting reliability and availability of the unit (140). An embodiment of the present invention provides an inlet system (160) for an exhaust gas recirculation system (100). This inlet system (160) may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream (125) flows within the inlet system (160).
申请公布号 EP2184464(A2) 申请公布日期 2010.05.12
申请号 EP20090173864 申请日期 2009.10.23
申请人 GENERAL ELECTRIC COMPANY 发明人 DRAPER, SAM D.;BYRD, DOUGLAS S.;SCHOTT, CARL G.;CHILLAR, RAHUL J.;TOPRANI, AMIT S.
分类号 F02C1/00;F02C3/34;F02C7/05 主分类号 F02C1/00
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