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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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