• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2018, Vol. 54 ›› Issue (14): 74-81.doi: 10.3901/JME.2018.14.074

• 材料科学与工程 • 上一篇    下一篇

偏心载荷作用下螺栓连接结构的松动行为研究

杜永强, 刘建华, 刘学通, 蔡振兵, 彭金方, 朱旻昊   

  1. 西南交通大学牵引动力国家重点实验室 成都 610031
  • 收稿日期:2017-09-06 修回日期:2017-12-09 出版日期:2018-07-20 发布日期:2018-07-20
  • 通讯作者: 刘建华(通信作者),男,1987年出生,博士。主要研究方向为微动摩擦学、紧固件连接设计。E-mail:jianhua-liu@sujtu.edu.cn
  • 作者简介:杜永强,男,1991年出生。主要研究方向为微动疲劳、紧固件连接设计。E-mail:duyongqiang_0806@163.com
  • 基金资助:
    国家自然科学基金(U1534209,51705434)和牵引动力国家重点实验室自主课题(2016TPL-Z03)资助项目。

Research on Self-Loosening Behavior of Bolted Joints under Eccentric Excitation

DU Yongqiang, LIU Jianhua, LIU Xuetong, CAI Zhenbing, PENG Jinfang, ZHU Minhao   

  1. Traction Power State Key Laboratory, Southwest Jiaotong University, Chengdu 610031
  • Received:2017-09-06 Revised:2017-12-09 Online:2018-07-20 Published:2018-07-20

摘要: 在不同试验参数下,采用自主设计的螺栓加载装置,系统地开展偏心载荷作用下螺栓连接结构的松动试验。通过获取螺栓轴向力时变曲线,研究偏心载荷作用下螺栓连接结构的松动行为;运用三维显微镜(Optical microscope,OM)、扫描电子显微镜(Scanning electron microscope,SEM)以及X射线电子能谱仪(Energy dispersive X-ray,EDX)等分析方法对试验后的螺纹接触表面进行损伤形貌分析,深入讨论螺纹接触界面的微动运行行为(微观滑移和微动磨损)对螺栓松动的影响规律,进一步揭示螺栓连接结构的松动机理。结果表明:在偏心载荷作用下,螺栓轴向力表现出明显的下降趋势,但拧松力矩变化较小。螺栓轴向力的下降过程可以分为两个阶段:①由于螺纹接触表面粗糙峰被去除和连接结构的塑性变形,轴向力迅速下降;②由于材料的棘轮效应,塑性变形趋于安定极限,螺纹接触面之间的微动磨损导致螺栓轴向力缓慢下降。螺纹接触面之间的损伤机制主要表现为疲劳磨损,并伴随磨粒磨损和黏着磨损。此外,运用ABAQUS对试验过程进行数值模拟,其计算结果与试验结果相互吻合。

关键词: 螺栓连接结构, 偏心载荷, 松动机理, 微动磨损

Abstract: Based on a new bolt loosening test rig, the loosening tests of bolted joints subjected to eccentric excitation are carried out under various experimental parameters. According to the evolution curves of the axial force of the bolt, the self-loosening behavior of bolted joints under eccentric excitation is investigated. After the tests, the damage of threads is analyzed using OM (optical microscope), SEM (scanning electron microscope) and EDX (energy dispersive X-ray). The influences of fretting behavior (micro-slip and fretting wear) between the contact threads on self-loosening of bolted joints are discussed in depth, and the self-loosening mechanism of bolted joints is revealed in details. The results show that the axial force of the bolt decreased obviously, while the breakaway torque has no obvious change. The self-loosening process of a bolted joint can be divided into two stages:Firstly, the axial force of the bolt drops rapidly due to the removal of asperities on the contact surfaces and the plastic deformation. Secondly, because of the ratcheting of material, plastic deformation increases slowly, and fretting wear between contact surfaces is the main reason of the decrease of the axial force of the bolt. The main wear mechanisms of the contact surfaces between threads were delamination, abrasive wear and adhesive wear. In addition, numerical simulation was performed using ABAQUS, and the FE results are agreement with the experimental observations.

Key words: bolted joints, eccentric excitation, fretting wear, self-loosening mechanism

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