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    • 2. 发明申请
    • TURBOMACHINE WITH MIXED-FLOW STAGE AND METHOD
    • 具有混合流动阶段和方法的涡轮机
    • US20120057965A1
    • 2012-03-08
    • US13220119
    • 2011-08-29
    • Lorenzo BERGAMINIVittorio Michelassi
    • Lorenzo BERGAMINIVittorio Michelassi
    • F04D13/12
    • F04D31/00F04D3/00F04D7/04F04D13/12F04D29/181F04D29/183F04D29/22
    • In one embodiment, a turbomachine for imparting energy to a multiphase fluid is provided. The turbomachine comprises a casing having an inlet and an outlet; an axial stage part comprising at least one axial stage; a mixed-flow stage part comprising at least one mixed-flow stage fluidly connected to the axial stage part; and a centrifugal stage part comprising at least one centrifugal stage fluidly connected to the mixed-flow stage part. The axial stage is defined by an angle between an axial impeller outlet flow and an axis parallel to a rotational axis of the shaft having a value between 0° and 5°, the mixed-flow stage by an angle having a value between 5° and 80°, and the centrifugal stage by an angle having a value between 80° and 90°.
    • 在一个实施例中,提供了用于向多相流体施加能量的涡轮机。 涡轮机包括具有入口和出口的壳体; 包括至少一个轴向平台的轴向平台部分; 混流阶段部分,包括流体连接到所述轴向台部的至少一个混流阶段; 以及离心级部分,其包括流体连接到所述混合流动级部分的至少一个离心级。 轴向级由轴向叶轮出口流和平行于轴的旋转轴线的轴之间的角度限定,其角度在0°和5°之间,混合流动台的角度为5°和 80°,离心级角度为80°〜90°。