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Mechanical Analysis of a Pin Interference-Fitted Sheet under Tensile Loading

机译:拉伸载荷作用下销钉干涉薄板的力学分析

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摘要

Interference fit can lead to better fatigue behavior of mechanical fastened joints. To explore the fatigue enhancement mechanism of interference fit, an analytical model of an interference-fit pinned sheet under subsequent tensile loading is presented. This model is employed to correlate the bypass load with the external longitudinal tensile load of the sheet, and the range of the two forces. Three-dimensional (3D) finite element (FE) analysis is performed using ABAQUS and comparison between the results of the two models shows a good agreement. Analytical results reveal that the key to the reduction of the bypass load amplitude lies in the elastic deformation of connected members of interference-fitted joints and the contact between them. This effect is accomplished through the automatic adjustment of the contact at the interfaces of the pin and sheet. For a specific joint, the effective affecting range (EAR) of interference for external loading is dependent on the interference and stiffness of its members. Specifically, the bypass load amplitude can be reduced only when external loads intersect EAR with a nonempty subset. If exerted loads are entirely within EAR, the bypass load amplitude can be minimized and the reduction ratio depends solely upon the stiffness of the connected members. It is also concluded that taking into consideration the external loads, especially its maximum value, is essential in the optimizing of interference. Finally, the optimum interference is deduced via the analytical model.
机译:过盈配合可导致机械紧固接头具有更好的疲劳性能。为了探讨过盈配合的疲劳增强机理,提出了过盈配合下张紧载荷作用下的过盈配合固定板的解析模型。该模型用于将旁路载荷与板的外部纵向拉伸载荷以及两个力的范围相关联。使用ABAQUS进行了三维(3D)有限元(FE)分析,并且两个模型的结果之间的比较显示出很好的一致性。分析结果表明,减小旁路载荷幅值的关键在于过盈配合接头的连接构件的弹性变形以及它们之间的接触。这种效果是通过自动调整销钉和薄板的界面处的接触来实现的。对于特定的关节,外部载荷的有效干涉影响范围(EAR)取决于其构件的干涉和刚度。具体而言,只有当外部负载与EAR与非空子集相交时,才能减小旁路负载幅度。如果施加的负载完全在EAR范围内,则可以将旁路负载幅度最小化,并且减速比仅取决于所连接构件的刚度。还得出结论,在优化干扰时必须考虑外部负载,尤其是其最大负载。最后,通过分析模型得出最佳干扰。

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  • 来源
    《Journal of aerospace engineering》 |2016年第4期|04015085.1-04015085.9|共9页
  • 作者单位

    China Acad Engn Phys, Inst Syst Engn, Box 411,POB 919, Mianyang 621900, Peoples R China|Northwestern Polytech Univ, Key Lab Contemporary Design & Integrated Mfg, Xian 710072, Peoples R China;

    Northwestern Polytech Univ, Key Lab Contemporary Design & Integrated Mfg, Xian 710072, Peoples R China;

    China Acad Engn Phys, Inst Syst Engn, Box 411,POB 919, Mianyang 621900, Peoples R China;

    China Acad Engn Phys, Inst Syst Engn, Box 411,POB 919, Mianyang 621900, Peoples R China;

    Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Fatigue life; Mechanical joints; Interference fit; Analytical solutions; Stress amplitude; Fretting fatigue;

    机译:疲劳寿命;机械接头;过盈配合;解析解;应力振幅;微动疲劳;

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