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Device for testing load bearing detection of a secondary channel of a flight control actuator, and associated testing method

机译:用于测试飞行控制致动器的辅助通道的负载检测的装置以及相关的测试方法

摘要

The device has a tool (33) operably pressing against a zone of an element of a secondary path of a flight control actuator, and a lever arm (30) allowing the tool to press against the zone by tilting, so that the lever arm exerts one of traction and compression force on the secondary path. The lever arm is mounted pivotingly on a support (31) operably fastened on a structure that is mechanically independent of the secondary path. The tool comprises a set including two plates that are connected by two clamping screws (35a, 35b). An independent claim is also included for a method for testing a detector that operably detects loading of a secondary path of a flight control actuator.
机译:该装置具有可操作地压在飞行控制致动器的次级路径的元件的区域上的工具(33),以及允许臂通过倾斜而压在该区域上的杠杆臂(30),从而杠杆臂施加次级路径上的牵引力和压缩力之一。杠杆臂可枢转地安装在支撑件(31)上,该支撑件可操作地固定在机械上独立于次要路径的结构上。该工具包括一组,该组包括通过两个夹紧螺钉(35a,35b)连接的两个板。还包括用于测试检测器的方法的独立权利要求,该检测器可操作地检测飞行控制致动器的次级路径的负载。

著录项

  • 公开/公告号EP2332838B1

    专利类型

  • 公开/公告日2016-07-13

    原文格式PDF

  • 申请/专利权人 GOODRICH ACTUATION SYSTEMS SAS;

    申请/专利号EP20100194205

  • 发明设计人 MOULON THOMAS;TURPIN PIERRE;

    申请日2010-12-08

  • 分类号B64F5;B64C13/42;B64C13/28;B64C13/36;F16H25/20;

  • 国家 EP

  • 入库时间 2022-08-21 14:53:05

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