发明名称 DUCT FOR CHANGING DIRECTION OF FLOW, PARTICULARLY FOR TURBOCHARGER COMPRESSOR INLET
摘要 <p>A direction changing flow duct, for example, a compressor inlet duct (34) for a turbocharger compressor cover, wherein the direction of flow is made to change abruptly in a short distance. The direction changing segment is designed to provide a balanced output, optimize air flow, minimize pressure drop, and maintain compressor efficiency. This can be accomplished by providing a bulge (81, 83, 84) extending radially inwards into a first duct segment, outward bulges perpendicular to the inward bulge, for promoting flow attachment along the walls of the duct.</p>
申请公布号 WO2009052170(A2) 申请公布日期 2009.04.23
申请号 WO2008US79978 申请日期 2008.10.15
申请人 BORGWARNER INC.;ANSCHEL, PAUL;ROBY, STEPHEN 发明人 ANSCHEL, PAUL;ROBY, STEPHEN
分类号 F02B37/22;F02B33/44 主分类号 F02B37/22
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