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Load application device, load measuring device, and aircraft load application method

机译:载荷施加装置,载荷测量装置以及飞机载荷施加方法

摘要

The present invention aims to apply a vertical load to a specimen with high precision even if the specimen shifts horizontally. A load application device includes: a hydraulic actuator which applies a load to a specimen; a support structural body which supports the hydraulic actuator along a vertical direction; a horizontal guide surface which guides the support structural body along a horizontal direction; and a bearing which is interposed between the support structural body and the horizontal guide surface and bears the support structural body so as to be horizontally shiftable relative to the horizontal guide surface. This bearing includes a plurality of spherical bodies supported so as to be independently rollable, and the plurality of spherical bodies are held in contact with the support structural body or the horizontal guide surface.
机译:本发明的目的是即使样品水平移动,也能以高精度对样品施加垂直载荷。一种载荷施加装置,包括:液压致动器,其将载荷施加到样本;以及液压致动器。沿竖直方向支撑液压致动器的支撑结构体;水平引导面,其沿水平方向引导支撑结构体;轴承,其设置在支撑结构体与水平引导面之间,并以相对于水平引导面可水平移动的方式支撑支撑结构体。该轴承包括被支撑为能够独立滚动的多个球形体,并且多个球形体保持与支撑结构体或水平引导表面接触。

著录项

  • 公开/公告号US9995651B2

    专利类型

  • 公开/公告日2018-06-12

    原文格式PDF

  • 申请/专利权人 MITSUBISHI AIRCRAFT CORPORATION;

    申请/专利号US201514962886

  • 发明设计人 ISAMU NAKAGAWA;

    申请日2015-12-08

  • 分类号G01M13/04;B64F5/60;

  • 国家 US

  • 入库时间 2022-08-21 12:55:49

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