发明名称 Variable geometry turbocharger having internal bypass exhaust gas flow
摘要 Variable geometry turbochargers include a turbine housing having an exhaust gas inlet and outlet, a volute connected to the inlet, and typically a nozzle wall adjacent the volute. The turbine housing includes a bypass exhaust gas flow port disposed internally therein having an inlet opening positioned upstream from the turbine wheel, and a outlet opening positioned downstream from the turbine wheel. The inlet opening is exposed for facilitating bypass exhaust gas flow through the turbocharger when a respective vane is actuated or moved into an open position. The turbine housing may also include a specially configured nozzle wall terminal edge designed to work with vanes having a recessed underside surface to permit additional bypass exhaust gas flow within the turbocharger when the vanes are actuated in an open position.
申请公布号 US6729134(B2) 申请公布日期 2004.05.04
申请号 US20020178754 申请日期 2002.06.24
申请人 HONEYWELL INTERNATIONAL INC. 发明人 ARNOLD STEVEN DON;SLUPSKI KEVIN P.;WIERSMA ZANDRIE J.;BUNSIRISERT KELVIN K.
分类号 F01D9/02;F01D5/14;F01D5/18;F01D17/10;F01D17/16;F02B37/18;F02B37/24;F02C6/12;(IPC1-7):F02D23/00 主分类号 F01D9/02
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