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Shape measuring method of load stress estimation method and the columnar structure of fictitious equipment for support

机译:载荷应力估计方法的形状测量方法和虚拟支撑设备的柱状结构

摘要

PROBLEM TO BE SOLVED: To provide a method for accurately estimating a load stress of a support for an aerial facility through simple procedures.;SOLUTION: A load stress estimation method includes the steps of: measuring a surface shape of a support, using a three-dimensional shape measuring device of a range finding type from at least two measuring points which are separated from the support for an aerial facility at an azimuth angle 50° or more around the support and included within a range where a distance to the support is 0.2 times or more and 60 times or less as much as a height of the support; calculating a measurement centerline connecting a central position of a horizontal cross section of the support along a height direction of the support and a reference centerline extending perpendicularly through a center at a ground edge position of the support from the measured shape information of the support; calculating a horizontal displacement value at each height position of the support by comparing the measurement centerline with the reference centerline; and using the displacement value to refer to an analytical curve on the basis of measurement data of an article equal to the support, thereby estimating a load stress of the support as a measurement target.;COPYRIGHT: (C)2012,JPO&INPIT
机译:要解决的问题:提供一种通过简单的程序准确估算航空设施支撑物的负载应力的方法;解决方案:负载应力估算方法包括以下步骤:使用三种方法测量支撑物的表面形状一种测距型三维形状测量装置,它至少有两个测量点,这些测量点与航空设施的支架以50°的方位角分开。在支撑物周围为大于等于支撑物高度的0.2倍以上且在支撑物高度的60倍以下的范围内。根据测得的支撑件的形状信息,计算连接支撑件的水平横截面的中心位置沿支撑件的高度方向的测量中心线和垂直延伸穿过支撑件的底边缘位置的中心的基准中心线;通过将测量中心线与参考中心线进行比较来计算支撑件的每个高度位置处的水平位移值;并以与支撑体相等的物品的测量数据为基础,利用位移值参考分析曲线,从而估算作为测量目标的支撑体的负荷应力。版权所有:(C)2012,JPO&INPIT

著录项

  • 公开/公告号JP5556598B2

    专利类型

  • 公开/公告日2014-07-23

    原文格式PDF

  • 申请/专利权人 東京電力株式会社;

    申请/专利号JP20100246656

  • 发明设计人 市場 幹之;新留 裕也;

    申请日2010-11-02

  • 分类号G01L1/00;G01B11/16;

  • 国家 JP

  • 入库时间 2022-08-21 16:14:44

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