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Bladed stator stage of a compressor, corresponding compressor and method of retention of vanes in such a stator stage

机译:压缩机的叶片式定子级,相应的压缩机以及将叶片保持在这种定子级中的方法

摘要

The stage has series of vanes (3), whose heads (4) are fixed at an external shell (1), and feet (5) are fixed at an internal shell (2). The internal shell comprises a series of cutouts receiving the feet, where the feet are projected towards an internal face of the internal shell. Spiral rings (6, 6') are housed in an opening of the each vane to prevent the feet of the vane from being pulled out from the cutouts, respectively, and to form a connection between the feet, where the rings are made of spring steel. Independent claims are also included for the following: (1) a method for holding vanes of a rectifier stage of a compressor of an axial turbomachine (2) a method for fixing heads of vanes to an external shell.
机译:该平台具有一系列叶片(3),其头部(4)固定在外壳(1)上,而支脚(5)固定在内部外壳(2)上。内壳包括一系列容纳脚的切口,其中,脚朝着内壳的内表面突出。螺旋环(6、6')容纳在每个叶片的开口中,以防止叶片的支脚分别从切口中拔出,并在支脚之间形成连接,这些环由弹簧制成钢。还包括以下方面的独立权利要求:(1)一种用于固定轴向涡轮机的压缩机的整流器级的叶片的方法(2)一种用于将叶片的头部固定至外壳的方法。

著录项

  • 公开/公告号EP2204546B1

    专利类型

  • 公开/公告日2012-03-07

    原文格式PDF

  • 申请/专利权人 TECHSPACE AERO SA;

    申请/专利号EP20080172916

  • 发明设计人 PENALVER CASTRO ENRIQUE;CULOT YVES;

    申请日2008-12-24

  • 分类号F01D9/04;F01D25/24;

  • 国家 EP

  • 入库时间 2022-08-21 17:15:59

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