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Segmented composite shroud ring of an axial compressor

机译:轴流压缩机的分段式复合罩环

摘要

The shroud (8) has arc shape segments (8a, 8b) with an exterior surface including openings (10). The openings receive an end of a vane (4) of a stator. An end of the segments has sections (11a, 11b), whose profile corresponds to profile of an end of the vane, when the segment is placed on the vane of the stator so that a junction between the segments corresponds to the section of the vane. A connection at level of another junction between the vane and the segments is provided by an application of elastomer, during assembling the segments on the vane. The segments are made of a composite material e.g. material comprising a resin associated to carbon fibers and/or glass fibers.
机译:护罩(8)具有弧形段(8a,8b),其外表面包括开口(10)。开口容纳定子的叶片(4)的端部。当将分段放置在定子的叶片上时,分段的端部具有部分(11a,11b),其轮廓对应于叶片的端部的轮廓,使得分段之间的接合处对应于叶片的截面。 。在将叶片组装在叶片上的过程中,通过施加弹性体来提供叶片和叶片之间的另一接合处的水平连接。所述段由复合材料制成,例如包含与碳纤维和/或玻璃纤维结合的树脂的材料。

著录项

  • 公开/公告号EP2196629B1

    专利类型

  • 公开/公告日2018-05-16

    原文格式PDF

  • 申请/专利权人 SAFRAN AERO BOOSTERS SA;

    申请/专利号EP20080171385

  • 发明设计人 CORTEQUISSE JEAN-FRANÇOIS;

    申请日2008-12-11

  • 分类号F01D9/04;

  • 国家 EP

  • 入库时间 2022-08-21 13:19:29

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