首页> 外国专利> Turbine blade with internal cooling channels having variable cross section in flow direction, for local coolant flow control resulting in constant temperature profile

Turbine blade with internal cooling channels having variable cross section in flow direction, for local coolant flow control resulting in constant temperature profile

机译:带有内部冷却通道的涡轮机叶片在流动方向上具有可变的横截面,用于局部冷却剂流量控制,从而实现恒定的温度曲线

摘要

The cooling channels extend between blade foot and tip and contain esp. steam as coolant, and have a cross section, which varies in flow direction of the steam. They are formed as radial passages with circular cross section. Alternatively, the channels are formed by hollow spaces between radial grooves (50) in the inside of a wall (52) forming the blade (5), and have an insert (70) covering the grooves. The insert is a metal plate held pre-tensioned against rails (56) between two neighboring grooves.
机译:冷却通道在刀脚和刀尖之间延伸并包含esp。蒸汽作为冷却剂,其横截面沿蒸汽的流动方向变化。它们形成为具有圆形横截面的径向通道。替代地,通道由形成叶片(5)的壁(52)内部的径向凹槽(50)之间的中空空间形成,并具有覆盖凹槽的插入件(70)。插入件是一块金属板,该金属板预紧抵靠在两个相邻凹槽之间的导轨(56)上。

著录项

  • 公开/公告号DE19860787A1

    专利类型

  • 公开/公告日2000-07-06

    原文格式PDF

  • 申请/专利权人 ABB RESEARCH LTD. ZUERICH;

    申请/专利号DE19981060787

  • 发明设计人 HARASGAMA PRITH;JOHNSON BRUCE;

    申请日1998-12-30

  • 分类号F01D5/18;

  • 国家 DE

  • 入库时间 2022-08-22 01:42:22

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