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Turbine rotor blade row, turbine stage and axial flow turbine

机译:涡轮动叶片排,涡轮级和轴流式涡轮

摘要

A turbine rotor blade row includes: a plurality of turbine rotor blades disposed along a circumferential direction of a hub. An inter-blade flow channel has a first cross-sectional shape perpendicular to a radial direction of the hub at a first position in the radial direction, and a second cross-sectional shape perpendicular to the radial direction of the hub at a second position farther from the hub than the first position in the radial direction. The first cross-sectional shape has a throat portion between an inlet and an outlet of the inter-blade flow channel in an axial direction of the hub. An expression A1/B1A2/B2 is satisfied, where A1 and A2 are flow-channel widths of the first cross-sectional shape at the outlet of the inter-blade flow channel and at the throat portion, respectively, and A2 and B2 are flow-channel widths of the second cross-sectional shape at the outlet of the inter-blade flow channel and at the same position as the throat portion in the axial direction of the hub, respectively.
机译:涡轮转子叶片列包括:沿着轮毂的周向设置的多个涡轮转子叶片。叶片间流路在径向上的第一位置处具有与轮毂的径向垂直的第一截面形状,在更远的第二位置处具有与轮毂的径向垂直的第二截面形状。从轮毂开始比在径向上的第一位置更远。第一横截面形状在轮毂的轴向方向上在叶片间流动通道的入口和出口之间具有喉部。满足表达式A1 / B1> A2 / B2,其中A1和A2分别是叶片间流道出口和喉部处的第一横截面形状的流道宽度,A2和B2分别是在叶片间流动通道的出口处和在毂的轴向上与喉部相同的位置处的第二横截面形状的流动通道宽度。

著录项

  • 公开/公告号JP6396093B2

    专利类型

  • 公开/公告日2018-09-26

    原文格式PDF

  • 申请/专利权人 三菱重工業株式会社;

    申请/专利号JP20140131442

  • 发明设计人 ▲高▼田 亮;目黒 圭一;

    申请日2014-06-26

  • 分类号F01D5/14;

  • 国家 JP

  • 入库时间 2022-08-21 13:10:04

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