发明申请
US20030014972A1 Variable geometry turbocharger having internal bypass exhaust gas flow
有权
具有内部旁路废气流量的可变几何涡轮增压器
- 专利标题: Variable geometry turbocharger having internal bypass exhaust gas flow
- 专利标题(中): 具有内部旁路废气流量的可变几何涡轮增压器
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申请号: US10178754申请日: 2002-06-24
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公开(公告)号: US20030014972A1公开(公告)日: 2003-01-23
- 发明人: Steven Don Arnold
- 主分类号: F02D023/00
- IPC分类号: F02D023/00
摘要:
Variable geometry turbochargers comprise a turbine housing having an exhaust gas inlet and outlet, a volute connected to the inlet, and a nozzle wall adjacent the volute. A turbine wheel is carried within the turbine housing and is attached to a shaft. A plurality of movable vanes are disposed within the turbine housing adjacent the nozzle wall, and are positioned between the exhaust gas inlet and turbine wheel. 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 vanes are positioned adjacent respective bypass ports such that the inlet opening for each port is at least partially covered by a respective vane depending on vane placement. The inlet opening is exposed for facilitating bypass exhaust gas flow through the turbocharger when the respective vane is actuated or moved into an open position. The turbine housing may also comprise 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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