首页> 外国专利> Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector

Angular sector of a stator for a turbine engine compressor, a turbine engine stator, and a turbine engine including such a sector

机译:用于涡轮发动机压缩机的定子的角扇形,涡轮发动机定子以及包括这种扇形的涡轮发动机

摘要

A stator angular sector for a turbine engine compressor including: an outer shroud and an inner shroud, and at least one vane extending radially between the shrouds. The outer shroud includes first and second mounting mechanisms for mounting the stator angular sector on a casing of the engine, which mechanisms are oriented parallel to the axis in opposite directions and connected together by an intermediate portion. The outer shroud includes at least one axial end portion extending from the intermediate portion with which at least one damper-forming insert is configured to come into contact, such that beyond a given value for amplitude of vibration of the end portion, the damper insert and the end portion are configured to move relative to each other to vary total moving mass moving with the end portion, thereby modifying vibratory behavior of the end portion.
机译:一种用于涡轮发动机压缩机的定子角扇区,其包括:外罩和内罩,以及在罩之间径向延伸的至少一个叶片。外罩包括用于将定子角部区段安装在发动机的壳体上的第一安装机构和第二安装机构,这些机构平行于轴线在相反方向上定向并且通过中间部分连接在一起。所述外罩包括从所述中间部分延伸的至少一个轴向端部,所述至少一个阻尼器形成插件构造成与所述中间部分接触,使得所述阻尼器插件和所述端部的振动幅度超过给定值。端部构造成相对于彼此移动以改变随端部移动的总移动质量,从而改变端部的振动行为。

著录项

  • 公开/公告号US9228449B2

    专利类型

  • 公开/公告日2016-01-05

    原文格式PDF

  • 申请/专利权人 YVON CLOAREC;

    申请/专利号US201113805211

  • 发明设计人 YVON CLOAREC;

    申请日2011-06-16

  • 分类号F01D25/04;F01D25/06;F04D29/66;F01D5/26;F01D9/04;F01D25/24;F01D5/22;

  • 国家 US

  • 入库时间 2022-08-21 14:27:58

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