首页> 外文期刊>Aerospace science and technology >Pre-tensioning effect on fatigue life of bolted shear joints
【24h】

Pre-tensioning effect on fatigue life of bolted shear joints

机译:预紧对螺栓剪切接头疲劳寿命的影响

获取原文
获取原文并翻译 | 示例
       

摘要

A number of experimental studies have demonstrated that pre-tensioning fasteners significantly increases the fatigue life of shear joints. Fatigue life prediction for clamped joints is still a complex and unresolved issue because of the mixed nature of load transfer, which partly occurs by frictional forces. This article presents a calculation method based on a multiaxial-type critical-plane criterion, which determines the fatigue life and fatigue crack initiation site. For this purpose, the values of hydrostatic pressure and amplitude of maximum alternating shear stress on a critical octahedral plane are determined at each point of the structure and for each loading increment, and are used to predict the fatigue life of the joint. A dedicated experimental study was conducted within materials & processes airbus laboratory to validate the numerical results. In addition, a dimensionless parameter Rs is introduced to quantify the proportion of load transferred by friction and by bearing of the bolt, and allows the optimal preload to be approximated, above which value more clamping should not give further improvement. This value characterizes the shift of the crack location from the net section to the outside of the compressed area.
机译:许多实验研究表明,预张紧的紧固件可显着延长剪切接头的疲劳寿命。由于载荷传递的混合特性(部分由摩擦力产生),对于夹紧接头的疲劳寿命预测仍然是一个复杂且尚未解决的问题。本文提出了一种基于多轴型临界面准则的计算方法,该方法确定了疲劳寿命和疲劳裂纹萌生点。为此,在结构的每个点和每个载荷增量中确定静水压力值和临界八面体平面上的最大交替剪切应力的幅度,并用于预测接头的疲劳寿命。在材料和过程空中客车实验室内进行了专门的实验研究,以验证数值结果。此外,引入了无量纲参数Rs来量化由摩擦和螺栓轴承传递的载荷比例,并允许近似最佳预载荷,在该值之上,更多的夹紧不应给出进一步的改进。该值表征了裂纹位置从净截面到压缩区域外部的位移。

著录项

  • 来源
    《Aerospace science and technology》 |2014年第7期|36-43|共8页
  • 作者单位

    Institut Clement Ader Impasse Didier Daurat Prolongee, 31400 Toulouse Cedex 04, France,Airbus Operations SAS, 316 Route de Bayonne, 31060 Toulouse Cedex 9, France;

    Airbus Operations SAS, 316 Route de Bayonne, 31060 Toulouse Cedex 9, France;

    Institut Clement Ader Impasse Didier Daurat Prolongee, 31400 Toulouse Cedex 04, France;

    Institut Clement Ader Impasse Didier Daurat Prolongee, 31400 Toulouse Cedex 04, France;

    Institut Clement Ader Impasse Didier Daurat Prolongee, 31400 Toulouse Cedex 04, France;

    Airbus Operations SAS, 316 Route de Bayonne, 31060 Toulouse Cedex 9, France;

  • 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 joints; Shear joint; Preload; Finite element analysis; Multiaxial criteria;

    机译:疲劳关节;剪力接头预载有限元分析;多轴标准;
  • 入库时间 2022-08-18 02:32:23

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号