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Mixed axial turbine engine compressor stator.

机译:混合轴向涡轮发动机压缩机定子。

摘要

The invention relates to a stator for a low pressure compressor of an axial turbomachine. The stator comprises an annular row of stator vanes with connecting vanes (38), and support vanes (36) grouped together in bladed boxes (40). The boxes (40) include internal platforms (42) and external platforms (44); they are entirely produced by additive manufacturing based on titanium powder. The stator shows a circular internal ferrule (32) formed by the internal platforms (42) of the vanes of the boxes and the internal ferrule segments (46) attached to the connecting vanes (38). The internal platforms (42) include pairs of mating surfaces for interlocking the ferrule segments therein by abutting and sliding against the mating surfaces. The contact surfaces are perpendicular to the axis of rotation and form axial stops.
机译:用于轴向涡轮机的低压压缩机的定子技术领域本发明涉及一种用于轴向涡轮机的低压压缩机的定子。定子包括一排环形的定子叶片,该定子叶片具有连接叶片(38)和支撑叶片(36),这些叶片在叶片盒(40)中组合在一起。盒子(40)包括内部平台(42)和外部平台(44)。它们完全通过基于钛粉的增材制造而生产。定子示出了圆形的内部套圈(32),该圆形的内部套圈(32)由箱的叶片的内部平台(42)和附接到连接叶片(38)的内部套圈段(46)形成。内部平台(42)包括成对的配合表面,用于通过邻接并抵靠配合表面滑动而将套圈段互锁在其中。接触表面垂直于旋转轴并形成轴向挡块。

著录项

  • 公开/公告号BE1022361B1

    专利类型

  • 公开/公告日2016-03-17

    原文格式PDF

  • 申请/专利权人 SAFRAN AERO BOOSTERS S.A.;

    申请/专利号BE20140000806

  • 发明设计人 CORTEQUISSE JEAN-FRANÇOIS;

    申请日2014-11-06

  • 分类号F01D9/04;F01D25/24;

  • 国家 BE

  • 入库时间 2022-08-21 14:27:33

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