首页> 外国专利> CONNECTING ROD FOR AERONAUTICAL MECHANISM AND AERONAUTICAL MECHANISM COMPRISING SUCH A CONNECTING ROD

CONNECTING ROD FOR AERONAUTICAL MECHANISM AND AERONAUTICAL MECHANISM COMPRISING SUCH A CONNECTING ROD

机译:用于气动机构的连接杆以及包括这种连接杆的气动机构

摘要

A connecting rod for an aeronautical actuator system, having one shaft transmitting forces applied in tension and/or compression along a longitudinal axis of the rod. When the connecting rod is in service, an elastically deformable element connected to the shaft is configured to react to the forces applied to the shaft, and displays elastic deformation when effected by these forces. The deformable element has a peripheral part rigidly connected to a member of the rod in which the shaft is slidably mounted. Measurement means associated with the deformable element determine the forces. The measurement means is partially housed in the deformable element. The deformable element includes a central part elongated along the longitudinal axis, which is rigidly connected to the shaft and in which the measurement means are at least partially housed. An intermediate part runs transversally to the central part and connects the central part and the peripheral part.
机译:一种用于航空致动器系统的连杆,其一根轴传递沿所述杆的纵轴施加拉力和/或压缩力的力。当连杆在使用中时,连接至轴的可弹性变形的元件构造成对施加于轴的力起反作用,并且在这些力的作用下显示出弹性变形。可变形元件具有刚性地连接到杆的构件的外围部分,轴可滑动地安装在杆的构件中。与可变形元件相关的测量装置确定力。测量装置部分地容纳在可变形元件中。可变形元件包括沿纵向轴线延伸的中央部分,该中央部分刚性地连接至轴并且测量装置至少部分地容纳在该中央部分中。中间部分横向于中央部分延伸并且连接中央部分和外围部分。

著录项

  • 公开/公告号EP2612044A1

    专利类型

  • 公开/公告日2013-07-10

    原文格式PDF

  • 申请/专利权人 FLY BY WIRE SYSTEMS FRANCE;

    申请/专利号EP20110764814

  • 发明设计人 BOUILLOT FRANCK;MILORD CEDRIC;

    申请日2011-08-30

  • 分类号F16C7/04;G01L5/10;

  • 国家 EP

  • 入库时间 2022-08-21 16:29:20

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