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首页> 外文期刊>Journal of engineering materials and technology >Fatigue Damage Analysis of Double-Lap Bolted Joints Considering the Effects of Hole Cold Expansion and Bolt Clamping Force
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Fatigue Damage Analysis of Double-Lap Bolted Joints Considering the Effects of Hole Cold Expansion and Bolt Clamping Force

机译:考虑孔冷胀和夹紧力影响的双搭螺栓连接疲劳损伤分析

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摘要

Hole cold expansion and bolt clamping force are usually applied to improve the fatigue performance of bolted joints. In order to investigate the effects of hole cold expansion and bolt clamping force and reveal the mechanism of these two factors on the fatigue damage of bolted joint, a continuum damage mechanics (CDM) based approach in conjunction with the finite element method is used. The damage-coupled Voyiadjis plasticity constitutive model is used to represent the material behavior, which is implemented by user material subroutine in ABAQUS. The elasticity and plasticity damage evolutions of the material are described by the stress-based and plastic-strain-based equations, respectively. The fatigue damage of joint is calculated using ABAQUS cycle by cycle. The fatigue lives of double-lap bolted joints with and without clamping force at different levels of hole cold expansion are all obtained. The characteristics of fatigue damage corresponding to the different conditions are presented to unfold the influencing mechanism of these two factors. The predicted fatigue lives and crack initiation locations are in good agreement with the experimental results available in the literature. The beneficial effects of hole cold expansion and bolt clamping force on the fatigue behavior of bolted joint are presented in this work.
机译:通常使用孔冷膨胀和螺栓夹紧力来改善螺栓连接的疲劳性能。为了研究孔的冷膨胀和螺栓夹紧力的影响,并揭示这两个因素对螺栓接头疲劳损伤的机理,采用了基于连续损伤力学(CDM)的有限元方法。损伤耦合的Voyiadjis可塑性本构模型用于表示材料行为,该模型由ABAQUS中的用户材料子例程实现。材料的弹性和塑性损伤演化分别通过基于应力和基于塑性应变的方程式描述。使用ABAQUS逐周期计算关节的疲劳损伤。在不同的孔冷膨胀水平下,均获得了带和不带夹紧力的双搭接螺栓连接的疲劳寿命。提出了不同条件下的疲劳损伤特征,以揭示这两个因素的影响机理。预测的疲劳寿命和裂纹萌生位置与文献中提供的实验结果非常吻合。这项工作提出了孔冷膨胀和螺栓夹紧力对螺栓连接疲劳性能的有益影响。

著录项

  • 来源
    《Journal of engineering materials and technology》 |2017年第2期|021007.1-021007.10|共10页
  • 作者单位

    School of Aeronautics Science and Engineering, Beihang University, Beijing 100191, China;

    Computational Solid Mechanics Laboratory, Department of Civil and Environmental Engineering, Louisiana State University, Baton Rouge, LA 70803;

    School of Aeronautics Science and Engineering, Beihang University, Room D604, New Main Building, 37th Xueyuan Road, Beijing 100191, China Computational Solid Mechanics Laboratory, Department of Civil and Environmental Engineering, Louisiana State University, Baton Rouge, LA 70803;

    School of Aeronautics Science and Engineering, Beihang University, Beijing 100191, China;

    School of Aeronautics Science and Engineering, Beihang University, Beijing 100191, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    fatigue damage; double-lap bolted joints; hole cold expansion; bolt clamping force; continuum damage mechanics; finite element;

    机译:疲劳损伤双搭螺栓连接;孔冷膨胀螺栓夹紧力;连续损伤力学;有限元;

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