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Blade ring for flow machine, particularly for gas turbine, has hardened reinforcement on inner shroud, where reinforcement is closed in circumferential direction

机译:流量机的叶片环,特别是燃气轮机的叶片环,在内罩上具有硬化的加强件,加强件在圆周方向上是封闭的

摘要

The blade ring (10) has a hardened reinforcement on an inner shroud (16), where the reinforcement is closed in circumferential direction. The reinforcement has a closed hollow profile. The reinforcement is formed as multi-part having multiple reinforcement portions. The inner shroud and the reinforcement portions are formed of different material and with different manufacturing method.
机译:叶片环(10)在内部护罩(16)上具有硬化的加强件,该加强件在圆周方向上是封闭的。加强件具有封闭的空心轮廓。加强件形成为具有多个加强部的多部分。内罩和加强部分由不同的材料和不同的制造方法形成。

著录项

  • 公开/公告号DE102009042029A1

    专利类型

  • 公开/公告日2011-03-24

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES GMBH;

    申请/专利号DE20091042029

  • 发明设计人 WEIDMANN WILFRIED;

    申请日2009-09-17

  • 分类号F01D5/22;F01D9/04;

  • 国家 DE

  • 入库时间 2022-08-21 17:47:42

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