首页> 外国专利> FATIGUE ANALYSIS METHOD OF CUTOUT PANEL MODEL USING RELATION BETWEEN MAXIMUM AND MINIMUM PRINCIPAL STRESSES

FATIGUE ANALYSIS METHOD OF CUTOUT PANEL MODEL USING RELATION BETWEEN MAXIMUM AND MINIMUM PRINCIPAL STRESSES

机译:基于最大与最小主应力关系的剪力板模型疲劳分析方法

摘要

The present invention relates to a fatigue analysis method of a cutout panel model using a relation between a maximum and minimum principal stresses includes: a step of acquiring data with respect to a ratio of a sample peak principal stress in accordance with a ratio of a sample principle stress of the model including an open hole; a step of acquiring an interaction formula with respect to the ratio of the sample peak principal stress in accordance with the ratio of the sample principal stress by performing curve fitting using data; a step of calculating the peak principal stress with respect to load conditions by a finite-element analysis of the model; a step of calculating the ratio of the peak principal stress with respect to the load conditions, and then acquiring the ratio of the corresponding principal stress based on the interaction formula; a step of calculating a reference stress and a stress concentration factor based on the ratio of the principal stress and the ratio of the peak principal stress; and a step of performing a fatigue analysis of the model based on the reference stress and the stress concentration factor. The fatigue analysis method of the cutout panel model using the relation between the maximum and minimum principal stresses in accordance with the present invention is capable of saving time and resources by calculating the stress concentration factor based on the relation between the maximum and minimum principal stresses without performing an existing method, and then calculating the principal stress based on the stress concentration factor; thereby obtaining an effect of improving efficiency.;COPYRIGHT KIPO 2017
机译:本发明涉及一种利用最大主应力与最小主应力之间的关系的切口面板模型的疲劳分析方法,该方法包括:根据样品的比例获取关于样品峰值主应力的比例的数据的步骤。模型的主应力,包括开孔;通过利用数据进行曲线拟合,求出与试样主应力之比相对应的试样峰值主应力之比的相互作用式的步骤。通过模型的有限元分析来计算相对于载荷条件的峰值主应力的步骤;计算峰值主应力相对于载荷条件的比率,然后根据相互作用公式获得相应主应力的比率的步骤;根据主应力之比与峰值主应力之比计算参考应力和应力集中系数的步骤;根据参考应力和应力集中系数对模型进行疲劳分析的步骤。根据本发明的利用最大和最小主应力之间的关系的切口面板模型的疲劳分析方法能够通过基于最大和最小主应力之间的关系来计算应力集中系数来节省时间和资源。执行现有方法,然后基于应力集中因子计算主应力;从而获得提高效率的效果。; COPYRIGHT KIPO 2017

著录项

  • 公开/公告号KR20170104221A

    专利类型

  • 公开/公告日2017-09-15

    原文格式PDF

  • 申请/专利权人 KOREA AEROSPACE INDUSTRIES LTD.;

    申请/专利号KR20160026934

  • 发明设计人 SHIN IN SOOKR;

    申请日2016-03-07

  • 分类号G01N3/06;G01N3/04;

  • 国家 KR

  • 入库时间 2022-08-21 13:26:39

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