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Axial-flow turbine having stepped portion formed in axial-flow turbine passage

机译:轴流式涡轮机,在轴流式涡轮机通道中形成有台阶部

摘要

There is provided an axial-flow turbine comprising an exhaust chamber; a turbine including multiple stage rotor blades, said multiple stage rotor blade including terminal stage rotor blades; an annular diffuser located between the turbine and the exhaust chamber; and an annular axial-flow turbine passage defined by the turbine, the diffuser and the exhaust chamber, wherein fluid flows through the axial-flow turbine passage toward the exhaust chamber, and an annular stepped portion which inwardly projects in a radial direction is formed on the portion of an inner wall of the axial-flow turbine passage that is located on the downstream side of a trailing edge of a tip portion of the terminal stage rotor blades provided in the flow direction of the fluid. In the stepped portion, a projecting portion which inwardly projects in a radial direction may be provided.
机译:本发明提供一种轴流式涡轮机,其包括排气室。一种涡轮,包括多级转子叶片,所述多级转子叶片包括末端级转子叶片;位于涡轮和排气室之间的环形扩压器;由涡轮,扩散器和排气室限定的环形轴流涡轮通道,其中流体通过轴流涡轮通道流向排气室,并且在径向上向内突出的环形台阶部分形成在环形台阶上。轴流式涡轮机通道的内壁的,位于沿流体的流动方向设置的终端级动叶片的前端的后缘的下游侧的部分。在台阶部分中,可以设置在径向方向上向内突出的突出部分。

著录项

  • 公开/公告号US2002159886A1

    专利类型

  • 公开/公告日2002-10-31

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;

    申请/专利号US20020079853

  • 发明设计人 TAKASHI HIYAMA;EISAKU ITO;

    申请日2002-02-22

  • 分类号F01D25/30;

  • 国家 US

  • 入库时间 2022-08-22 00:51:45

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