首页> 外国专利> Guide vane for a turbomachine, guide vane cascade, and method for manufacturing a guide vane or a guide vane cascade

Guide vane for a turbomachine, guide vane cascade, and method for manufacturing a guide vane or a guide vane cascade

机译:用于涡轮机的导向叶片,导向叶片叶栅以及用于制造导向叶片或导向叶片叶栅的方法

摘要

A guide vane for a turbomachine axially pivotably coupled to a radially outwardly disposed flow-limiting wall and to a radially inwardly disposed inner ring of the turbomachine; and a trailing edge gap being formed between an upper trailing edge of the guide vane and the flow-limiting wall and/or between a lower trailing edge of the guide vane and the inner ring; the upper trailing edge and/or the lower trailing edge of the guide vane having at least one air outlet opening for an air outflow for forming an air curtain for at least partially sealing the trailing edge gap in the area of the upper trailing edge and/or the lower trailing edge in the area of the lower trailing edge. Also, a guide vane cascade, as well as a method for manufacturing a guide vane or a guide vane cascade.
机译:用于涡轮机的导向叶片轴向地可枢转地联接到径向向外设置的限流壁和涡轮机的径向向内设置的内环;在导向叶片的上尾缘与限流壁之间和/或在导向叶片的下尾缘与内环之间形成有后缘间隙。导向叶片的上后缘和/或下后缘具有至少一个用于空气流出的空气出口,用于形成空气幕,以至少部分地密封上后缘区域中的后缘间隙和/或下后缘区域中的下后缘。另外,导向叶片叶栅以及用于制造导向叶片或导向叶片叶栅的方法。

著录项

  • 公开/公告号US10060439B2

    专利类型

  • 公开/公告日2018-08-28

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES AG;

    申请/专利号US201715446241

  • 发明设计人 GEORG ZOTZ;

    申请日2017-03-01

  • 分类号F01D11;F01D11/08;F01D5/18;F01D5/20;F04D29/16;F04D19;F04D29/56;F04D29/54;B23K26/342;B33Y10;B33Y80;B22F3/105;B22F5/04;B23K101;

  • 国家 US

  • 入库时间 2022-08-21 13:03:26

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