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Flow divider for radial-axial intake housing - is located in turbine entry, in central banking-up point of housing flow

机译:径向-轴向进气壳体的分流器-位于涡轮入口处,在壳体流动的中央倾斜点

摘要

The flow divider (2) is located in the turbine entry, opposite to the intake and in front of the first guide row (3); resp. in the compressor entry, opposite to the intake and in front of the ribs. The flow divider is positioned in the central banking-up point of the housing flow. The divider has a thick-head profile with max. profile thickness and straight median line. The rear face of the flow divider is at right angles to the rotor shaft at a distance to the first guide row resp. ribs. There is free play between inner divider face and housing wall. The chord length of the divider decreases outwards. The front face of the divider is inclined. USE/ADVANTAGE - Rotating thermal machine. Large stabilization of flow, overflow is prevented/more difficult.
机译:分流器(2)位于涡轮机入口,与进气口相对,并位于第一导向排(3)的前面;分别在压缩机入口处,与进气口相对且在肋骨的前面。分流器位于外壳流的中央堆积点。分频器的粗头轮廓最大为轮廓厚度和正中线。分流器的后表面与转子轴成直角,与第一导向排相对应。肋骨。内隔板表面和外壳壁之间有自由运动。分隔线的和弦长度向外减小。分隔器的正面倾斜。使用/优点-旋转热机。较大的流量稳定度,防止/防止溢流。

著录项

  • 公开/公告号DE4328186A1

    专利类型

  • 公开/公告日1994-04-28

    原文格式PDF

  • 申请/专利权人 ASEA BROWN BOVERI AG BADEN AARGAU CH;

    申请/专利号DE19934328186

  • 发明设计人 KREITMEIER FRANZ BADEN CH;

    申请日1993-08-21

  • 分类号F01D9/06;F02C7/00;

  • 国家 DE

  • 入库时间 2022-08-22 04:35:39

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