SCULPTED IMPELLER
    1.
    发明申请
    SCULPTED IMPELLER 审中-公开
    压片机

    公开(公告)号:WO2012161849A1

    公开(公告)日:2012-11-29

    申请号:PCT/US2012/027557

    申请日:2012-03-02

    CPC classification number: F04D29/30

    Abstract: A system includes an impeller ( 10 ) having a plurality of impeller blades ( 12 ) coupled to an impeller hub body ( 14 ), wherein each impeller blade is sculpted having a nonlinear profile extending from a hub intersect surface of the impeller blade to a shroud intersect surface of the impeller blade.

    Abstract translation: 一种系统包括具有联接到叶轮毂体(14)的多个叶轮叶片(12)的叶轮(10),其中每个叶轮叶片被雕刻成具有从叶轮叶片的轮毂相交表面延伸到护罩的非线性轮廓 叶轮叶片的相交表面。

    NON-PERIODIC CENTRIFUGAL COMPRESSOR DIFFUSER
    2.
    发明申请
    NON-PERIODIC CENTRIFUGAL COMPRESSOR DIFFUSER 审中-公开
    非周期性离心压缩机扩压器

    公开(公告)号:WO2011096981A1

    公开(公告)日:2011-08-11

    申请号:PCT/US2010/058439

    申请日:2010-11-30

    CPC classification number: F04D29/444 F04D29/666 F05D2250/52

    Abstract: A system, in certain embodiments, includes a centrifugal compressor diffuser having a mounting surface and plurality of diffuser vanes extending from the mounting surface in an axial direction and forming an asymmetrical (e.g., non-periodic) pattern around the circumference of the diffuser. The asymmetrical pattern may be determined based upon characteristics of fluid flowing from an impeller across the diffuser and through a scroll of a centrifugal compressor.

    Abstract translation: 在某些实施例中,系统包括离心式压缩机扩散器,其具有安装表面和沿着轴向从安装表面延伸的多个扩散器叶片,并且围绕扩散器的圆周形成不对称(例如非周期性)图案。 可以基于从叶轮流过扩散器并通过离心式压缩机的涡旋件的流体的特性来确定不对称模式。

    CENTRIFUGAL COMPRESSOR DIFFUSER VANELET
    3.
    发明申请
    CENTRIFUGAL COMPRESSOR DIFFUSER VANELET 审中-公开
    离心式压缩机散热器风扇

    公开(公告)号:WO2011096980A1

    公开(公告)日:2011-08-11

    申请号:PCT/US2010/058429

    申请日:2010-11-30

    CPC classification number: F04D29/44 F04D29/444 F04D29/666 F05D2250/52

    Abstract: A system, in certain embodiments, includes a centrifugal compressor diffuser including a flow path having a first surface and a second surface defining opposite axial sides of the flow path. The centrifugal compressor diffuser also includes multiple vanes extending from the first surface to the second surface of the flow path. A first profile of each vane varies along an axial direction. The centrifugal compressor diffuser further includes multiple vanelets extending from the first surface toward the second surface in the axial direction. A first axial extent of each vanelet is less than a second axial extent of the flow path. In addition, a second profile of each vanelet varies along the axial direction and/or the vanelets form a non-periodic pattern around a circumference of the flow path.

    Abstract translation: 在某些实施例中,系统包括离心压缩机扩散器,其包括具有第一表面的流动路径和限定流动路径的相对的轴向侧面的第二表面。 离心压缩机扩散器还包括从流动路径的第一表面延伸到第二表面的多个叶片。 每个叶片的第一轮廓沿轴向方向变化。 离心压缩机扩散器还包括沿轴向从第一表面向第二表面延伸的多个小叶片。 每个叶片的第一轴向范围小于流动路径的第二轴向范围。 此外,每个小叶的第二轮廓沿着轴向方向变化,和/或小叶形成围绕流动路径的圆周的非周期性图案。

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