兰州理工大学学报 ›› 2024, Vol. 50 ›› Issue (2): 111-117.

• 建筑科学 • 上一篇    下一篇

销铰节点螺栓销轴常幅疲劳性能试验研究与仿真分析

焦晋峰*1,2, 樊丽轩2, 李渊2, 魏珍中3, 刘勇3   

  1. 1.吕梁学院 建筑与土木工程系, 山西 吕梁 033001;
    2.太原理工大学 土木工程学院, 山西 太原 030024;
    3.山东电力工程咨询院有限公司, 山东 济南 250013
  • 收稿日期:2021-06-22 出版日期:2024-04-28 发布日期:2024-04-29
  • 通讯作者: 焦晋峰(1979-),男,山西晋城人,博士,教授.Email:jiaojf_1@126.com
  • 基金资助:
    国家自然科学基金(12172244),山西省省筹资金资助回国留学人员科研项目(2023-175),山西省基础研究计划资助项目(202203021211184),山西省自然科技研究基金(202103021223105),吕梁市高层次科技人才引进计划专项项目(2023RC15)

Experimental study and simulation analysis on constant amplitude fatigue of the bolt pin in pinned connection

JIAO Jin-feng1,2, FAN Li-xuan2, LI Yuan2, WEI Zhen-zhong3, LIU Yong3   

  1. 1. College of Architecture and Civil Engineering, Lyuliang University, Lyuliang 033001, China;
    2. College of Civil Engineering, Taiyuan University of Technology, Taiyuan 030024, China;
    3. Shandong Electric Power Engineering Consulting Institute Co. Ltd., Jinan 250013, China
  • Received:2021-06-22 Online:2024-04-28 Published:2024-04-29

摘要: 为揭示空间结构销铰节点螺栓销轴常幅疲劳破坏机理、探清其疲劳强度影响因素,对M36螺栓销轴进行疲劳试验.基于自行设计的加载装置,进行了9个螺栓销轴的常幅疲劳试验;采用nCode疲劳仿真分析软件对其进行4因素共32个模型疲劳模拟参数化分析.试验结果和数值模拟表明:销铰节点中最大等效应力位于内外耳板与螺栓销轴交界处,且该处应力集中程度严重;在忽略试件初始缺陷和试验加载等不利因素下,数值模拟所得疲劳寿命部分高于相应疲劳试验寿命,并基于线性拟合得到了该螺栓销轴的S-N曲线和理论疲劳寿命估算公式;螺栓销轴常幅疲劳强度与加载应力比/螺栓直径两个参数正相关,与销孔间隙初始增长呈负相关,且与耳板间距基本无关;螺栓销轴常幅疲劳性能影响因素敏感性顺序为:销孔间隙→螺栓直径→应力比→耳板间距.

关键词: 空间结构, 螺栓销轴, 常幅疲劳, 数值模拟, 参数分析

Abstract: In order to reveal the constant amplitude fatigue failure mechanism of bolt pin shaft in pin hinge joint of spatial structure and explore the influencing factors of fatigue strength, the fatigue test of M36 bolt pin shaft was carried out. Based on the self-designed loading device, the constant amplitude fatigue tests of 9 bolt pin shafts were conducted. The nCode fatigue simulation analysis software was used to do parameterized analysis of 32 models with 4 factors for fatigue simulation. The results shows that the maximum equivalent stress in the pin hinge joint appears at the junction of the inner and outer padeye and the bolt pin shaft, where the stress concentration is serious. Neglecting unfavorable factors such as initial defects of the specimen and experimental loading, the fatigue life obtained from numerical simulation is partially higher than the corresponding fatigue test life. The S-N curve and theoretical fatigue life estimation formula of the bolt pin shaft are obtained based on linear fitting. The constant amplitude fatigue strength of bolt pin shaft is positively correlated with the loading stress ratio and bolt diameter, negatively correlated with the initial growth of pin hole clearance, and has nothing to do with the ear plate spacing. The sensitivity order of influencing factors of constant amplitude fatigue performance of bolt pin shaft is: the gap of pin hole, the bolt diameter, the loading stress ratio, the ear plate spacing.

Key words: space structure, bolt pin, constant amplitude fatigue, numerical simulation, parametric analysis

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