发明授权
US08047772B2 Variable geometry turbine for a turbocharger and method of controlling the turbine
失效
用于涡轮增压器的可变几何涡轮机和控制涡轮机的方法
- 专利标题: Variable geometry turbine for a turbocharger and method of controlling the turbine
- 专利标题(中): 用于涡轮增压器的可变几何涡轮机和控制涡轮机的方法
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申请号: US11886834申请日: 2005-03-25
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公开(公告)号: US08047772B2公开(公告)日: 2011-11-01
- 发明人: Dominque Petitjean , Phillippe Arnold , Jerome Mitka
- 申请人: Dominque Petitjean , Phillippe Arnold , Jerome Mitka
- 申请人地址: US NJ Morristown
- 专利权人: Honeywell International Inc.
- 当前专利权人: Honeywell International Inc.
- 当前专利权人地址: US NJ Morristown
- 代理机构: Alston & Bird LLP
- 国际申请: PCT/EP2005/003314 WO 20050325
- 国际公布: WO2006/102912 WO 20061005
- 主分类号: F01B25/02
- IPC分类号: F01B25/02 ; F01B25/10
摘要:
There is described a variable geometry turbine having a sliding element (5) for the control of the section throat of the turbine (1) by sliding movement along an axial direction of a turbine wheel (71). The turbine wheel operates to convert a flow of working fluid into mechanical energy. At least one bypass channel (51) is defined in the sliding element (5). The bypass channel is further connected to a turbine wheel outlet area (79) downstream of the turbine wheel for selectively guiding an excess flow of working fluid past the turbine wheel (71), so as to control the operation of the turbine. A use of the variable geometry turbine with a turbocharger for an engine and a method for controlling such turbine is also described.
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