发明名称 TURBOCHARGER COMPRESSOR INLET FLOW CONTROL
摘要 Systems and methods for controlling compressor inlet flow in a turbocharger of an engine are described. In one example, a method for controlling a compressor inlet flow of an engine turbocharger system comprises: directing air from a high pressure source to an inlet upstream of a compressor wheel via a conduit coupled to the inlet and the high pressure source, where the conduit is obliquely coupled to the inlet.
申请公布号 US2013232971(A1) 申请公布日期 2013.09.12
申请号 US201213418207 申请日期 2012.03.12
申请人 MIAZGOWICZ KEITH D.;KARIM AHSANUL;PAYNE KEVIN;CHRISTIAN ADAM MICHAEL;FORD GLOBAL TECHNOLOGIES, LLC 发明人 MIAZGOWICZ KEITH D.;KARIM AHSANUL;PAYNE KEVIN;CHRISTIAN ADAM MICHAEL
分类号 F02D23/00;F02B33/32;F02M25/07 主分类号 F02D23/00
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