SECTOR-DIVIDED TURBINE ASSEMBLY WITH AXIAL PISTON VARIABLE-GEOMETRY MECHANISM
    3.
    发明申请
    SECTOR-DIVIDED TURBINE ASSEMBLY WITH AXIAL PISTON VARIABLE-GEOMETRY MECHANISM 审中-公开
    具有轴向活塞可变几何机构的分体式涡轮机组件

    公开(公告)号:WO2005040560A1

    公开(公告)日:2005-05-06

    申请号:PCT/IB2003/005142

    申请日:2003-10-24

    CPC classification number: F01D9/026 F01D17/143 F01D17/167 F05D2220/40

    Abstract: A turbine (40) for a turbocharger (10) has a turbine housing (41) defining a generally annular chamber (43) surrounding a turbine wheel (44), the chamber receiving exhaust gas for driving the turbine wheel. The chamber has dividing walls (46) that divide the chamber into a plurality of angular sectors (43a,43b), each fed with exhaust gas separately from the other sector(s). Vanes (52,53) located radially inwardly of the sectors for guiding flow into the turbine wheel include at least dividing vanes (52) that form extensions of the dividing walls (46) so as to extend the sector-division of the exhaust gas flow path all the way to the trailing edges of the dividing vanes. An axially slidable piston (48) is disposed radially inwardly of the sectors, and radially overlaps with the dividing vanes (52). The vanes either are mounted on fixed structure and are received in slots (49) in the piston, or are mounted on the piston and received in slots in fixed structure.

    Abstract translation: 用于涡轮增压器(10)的涡轮机(40)具有限定围绕涡轮机叶轮(44)的大致环形的室(43)的涡轮机壳体(41),所述室接收用于驱动涡轮机叶轮的废气。 该室具有分隔壁(46),该分隔壁将室分成多个角扇区(43a,43b),每个角扇区分别与另一个扇区供给废气。 位于扇形体径向向内以引导流入涡轮机叶轮的叶片(52,53)包括至少分隔叶片(52),其形成分隔壁(46)的延伸部分,以便延伸废气流的扇形分割 路径一直到分隔叶片的后缘。 轴向可滑动的活塞(48)设置在扇形体的径向内侧,并且与分隔叶片(52)径向重叠。 叶片安装在固定结构上并被容纳在活塞中的槽(49)中,或者安装在活塞上并被接收在固定结构的槽中。

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