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Contactless angular position sensor for measuring small angular position of control sleeve of aircraft, has magnetic sector intercepting apex angle that is greater than or equal to angular displacement and less than specific degrees

机译:非接触角位置传感器,用于测量飞机控制套的小角度位置,具有大于或等于角位移且小于特定角度的磁扇形截顶角

摘要

The sensor (1) has a magnetic structure (21) generating a magnetic field, and a magneto-sensitive element (11) secured to a stator assembly (10) or rotor assembly (20) and placed opposite to the structure. A magnetic sector (22) of the structure is arranged opposite to the element, where the sector comprises adjacent polar zones (23a, 23b) with equal size and alternated polarities. The sector intercepts apex angle in a plane orthogonal to a rotation axis (2), where the angle coinciding with the axis is greater than or equal to angular displacement (D) and less than 180 degrees.
机译:传感器(1)具有产生磁场的磁性结构(21)和固定在定子组件(10)或转子组件(20)上并与该结构相对的磁敏元件(11)。结构的磁扇区(22)与元件相对设置,其中该扇区包括具有相等大小和交替极性的相邻极性区域(23a,23b)。该扇形在与旋转轴(2)正交的平面中截取顶角,其中与该轴重合的角度大于或等于角位移(D)且小于180度。

著录项

  • 公开/公告号FR2950426A1

    专利类型

  • 公开/公告日2011-03-25

    原文格式PDF

  • 申请/专利权人 RATIER FIGEAC;

    申请/专利号FR20090004564

  • 发明设计人 ANTRAYGUE CEDRIC;

    申请日2009-09-24

  • 分类号G01D5/12;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:49

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