公开(公告)号：US20090169366A1

公开(公告)日：2009-07-02

申请号：US11886834

申请日：2005-03-25

申请人： Dominque Petitjean ,  Philippe Arnold ,  Jerome Mitka

发明人： Dominque Petitjean ,  Philippe Arnold ,  Jerome Mitka

IPC分类号： F01D17/00

CPC分类号： F02C6/12 ,  F01D17/105 ,  F01D17/143 ,  F02B37/18 ,  F05D2220/40

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.

摘要翻译： 描述了具有滑动元件（5）的可变几何涡轮机，用于通过沿着涡轮机叶轮（71）的轴向的滑动运动来控制涡轮机（1）的部分喉部。 涡轮机轮操作以将工作流体流转换成机械能。 至少一个旁通通道（51）限定在滑动元件（5）中。 旁路通道进一步连接到涡轮机叶轮下游的涡轮机叶轮出口区域（79），用于选择性地引导工作流体的过量流过涡轮机叶轮（71），以便控制涡轮机的运行。 还描述了使用具有用于发动机的涡轮增压器的可变几何涡轮机和用于控制这种涡轮机的方法。

公开(公告)号：US20090249785A1

公开(公告)日：2009-10-08

申请号：US12485698

申请日：2009-06-16

申请人： Lorrain Sausse ,  Raphael Hettinger ,  Dommique Petitjean ,  Gary Agnew ,  Philippe Arnold ,  Emmanuel Severin ,  Manual Dufin

发明人： Lorrain Sausse ,  Raphael Hettinger ,  Dommique Petitjean ,  Gary Agnew ,  Philippe Arnold ,  Emmanuel Severin ,  Manual Dufin

IPC分类号： F02D23/00

CPC分类号： F01D17/165 ,  F02C6/12 ,  F05D2220/40

摘要： A variable-nozzle turbocharger includes a turbine housing and a center housing, and a generally annular nozzle ring and an array of vanes rotatably mounted to the nozzle ring such that the vanes are rotatably adjustable for regulating exhaust gas flow to the turbine wheel. An elastically deformable member is disposed between a radially inwardly facing surface of the nozzle ring and a radially outwardly facing surface of the center housing, the elastically deformable member having a radially inner surface contacting the radially outwardly facing surface of the center housing and having a radially outer surface contacting the radially inwardly facing surface of the nozzle ring so as to radially center the nozzle ring relative to the center housing.

摘要翻译： 可变喷嘴涡轮增压器包括涡轮机壳体和中心壳体，以及大致环形的喷嘴环和可旋转地安装到喷嘴环的叶片阵列，使得叶片可旋转地调节以调节到涡轮机叶轮的排气流。 可弹性变形的构件设置在喷嘴环的径向向内的表面和中心壳体的径向向外的表面之间，弹性可变形构件具有接触中心壳体的径向向外的表面的径向内表面， 外表面接触喷嘴环的径向向内的表面，以使喷嘴环相对于中心壳体径向中心。

公开(公告)号：US08033109B2

公开(公告)日：2011-10-11

申请号：US12485698

申请日：2009-06-16

申请人： Lorrain Sausse ,  Raphael Hettinger ,  Dommique Petitjean ,  Gary Agnew ,  Philippe Arnold ,  Emmanuel Severin ,  Manual Dufin

发明人： Lorrain Sausse ,  Raphael Hettinger ,  Dommique Petitjean ,  Gary Agnew ,  Philippe Arnold ,  Emmanuel Severin ,  Manual Dufin

IPC分类号： F02D23/00 ,  F01D17/16 ,  F02C6/12 ,  F04D29/44

CPC分类号： F01D17/165 ,  F02C6/12 ,  F05D2220/40

摘要： A variable-nozzle turbocharger includes a turbine housing and a center housing, and a generally annular nozzle ring and an array of vanes rotatably mounted to the nozzle ring such that the vanes are rotatably adjustable for regulating exhaust gas flow to the turbine wheel. An elastically deformable member is disposed between a radially inwardly facing surface of the nozzle ring and a radially outwardly facing surface of the center housing, the elastically deformable member having a radially inner surface contacting the radially outwardly facing surface of the center housing and having a radially outer surface contacting the radially inwardly facing surface of the nozzle ring so as to radially center the nozzle ring relative to the center housing.

摘要翻译： 可变喷嘴涡轮增压器包括涡轮机壳体和中心壳体，以及大致环形的喷嘴环和可旋转地安装到喷嘴环的叶片阵列，使得叶片可旋转地调节以调节到涡轮机叶轮的排气流。 可弹性变形的构件设置在喷嘴环的径向向内的表面和中心壳体的径向向外的表面之间，弹性可变形构件具有接触中心壳体的径向向外的表面的径向内表面， 外表面接触喷嘴环的径向向内的表面，以使喷嘴环相对于中心壳体径向中心。