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Bayonet spacer retention system for variable turbine geometry vane packs

机译:卡口垫片固定系统,用于可变的涡轮几何叶片组

摘要

A variable geometry turbocharger includes a vane pack having rotatable vanes constrained by a pair of vane rings connected by a plurality of spacer connectors. The spacer connectors can include a spacer body for maintaining a minimum spacing between the vane rings. The spacer connectors are configured for bayonet mounting to at least one of the vane rings. To that end, the spacer connectors can include shaft portions extending from opposing sides of the spacer body. A plurality of transverse protrusions can extend outwardly from each shaft portion. Each shaft portion can be received in a respective in a vane ring. The spacer connectors can be rotated such that the transverse protrusions are offset from aperture portions that allow passage of the transverse portions, thereby retaining the vane rings in place in spaced relation. Such a system avoids close tolerances, press fits, expensive bolted joints or weld processes.
机译:可变几何形状的涡轮增压器包括叶片组,该叶片组具有由一对叶片环约束的可旋转叶片,该一对叶片环通过多个间隔连接器连接。间隔件连接器可包括用于保持叶片环之间的最小间隔的间隔件主体。间隔连接器被配置用于将卡口安装到至少一个叶片环上。为此,间隔器连接器可包括从间隔器主体的相对侧延伸的轴部分。多个横向突起可以从每个轴部分向外延伸。每个轴部分可以分别容纳在叶片环中。间隔器连接器可以旋转,使得横向突起从允许横向部分通过的孔部分偏移,从而以隔开的关系将叶片环保持在适当的位置。这样的系统避免了紧密的公差,压配合,昂贵的螺栓连接或焊接过程。

著录项

  • 公开/公告号US9856744B2

    专利类型

  • 公开/公告日2018-01-02

    原文格式PDF

  • 申请/专利权人 BORGWARNER INC.;

    申请/专利号US201314397969

  • 发明设计人 GEORGE E. HEDDY III;

    申请日2013-04-22

  • 分类号F01D17/16;F02B37/24;F02B39;

  • 国家 US

  • 入库时间 2022-08-21 12:55:41

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