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.
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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 |
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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