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钢桥面板纵肋与横隔板焊接细节疲劳开裂的加固研究

张清华 金通 李俊 卜一之

张清华, 金通, 李俊, 卜一之. 钢桥面板纵肋与横隔板焊接细节疲劳开裂的加固研究[J]. 西南交通大学学报, 2020, 55(1): 92-99. doi: 10.3969/j.issn.0258-2724.20170744
引用本文: 张清华, 金通, 李俊, 卜一之. 钢桥面板纵肋与横隔板焊接细节疲劳开裂的加固研究[J]. 西南交通大学学报, 2020, 55(1): 92-99. doi: 10.3969/j.issn.0258-2724.20170744
ZHANG Qinghua, JIN Tong, LI Jun, BU Yizhi. Study on Reinforcement for Fatigue Cracking of Rib-to-Diaphragm Welded Joints of Steel Bridge Deck[J]. Journal of Southwest Jiaotong University, 2020, 55(1): 92-99. doi: 10.3969/j.issn.0258-2724.20170744
Citation: ZHANG Qinghua, JIN Tong, LI Jun, BU Yizhi. Study on Reinforcement for Fatigue Cracking of Rib-to-Diaphragm Welded Joints of Steel Bridge Deck[J]. Journal of Southwest Jiaotong University, 2020, 55(1): 92-99. doi: 10.3969/j.issn.0258-2724.20170744

钢桥面板纵肋与横隔板焊接细节疲劳开裂的加固研究

doi: 10.3969/j.issn.0258-2724.20170744
基金项目: 国家自然科学基金(51578455,51778533,51178394);国家科技支撑计划(2011BAG07B03);中央高校基本科研业务费专项资金(2682014CX078)
详细信息
    作者简介:

    张清华(1975—),男,教授,研究方向为高性能钢与组合结构桥梁,E-mail:swjtuzqh@126.com

    通讯作者:

    卜一之(1961—),男,教授,研究方向为高性能钢与组合结构桥梁,E-mail:yizhibu@163.com

  • 中图分类号: U441.4

Study on Reinforcement for Fatigue Cracking of Rib-to-Diaphragm Welded Joints of Steel Bridge Deck

  • 摘要: 为研究钢桥面板疲劳开裂部位栓接角钢的加固方法,采用足尺模型试验对纵肋与横隔板焊接细节疲劳裂纹的加固效果进行研究,采用ANSYS建立了含有疲劳裂纹的有限元模型,并基于断裂力学理论对比研究疲劳裂纹不同长度条件下的加固效果. 研究结果表明:纵肋与横隔板焊接细节的疲劳裂纹起裂于焊趾并沿纵肋腹板扩展,采用栓接角钢加固后可以使开裂部位关键测点的主拉应力和裂尖各测点的应变分别降低56%和80%,能够有效抑制疲劳裂纹的扩展;栓接角钢加固后裂尖的应力强度因子幅值最少降低80%,裂纹扩展速率显著降低;对贯穿纵肋腹板前不同长度的疲劳裂纹进行加固,裂尖应力强度因子幅值均降低60%~90%,但随着疲劳裂纹长度的增加,栓接角钢的加固方法对裂纹扩展的抑制效果不断降低,加固时机的合理选取是影响加固效果的关键因素之一.

     

  • 图 1  纵肋与横隔板焊接细节处疲劳开裂模式

    Figure 1.  Fatigue cracking mode for structural details of rib-to-diaphragm

    图 2  纵肋与横隔板焊接细节装配式加固方式

    Figure 2.  Assembly rapid reinforcement for rib-to-diaphragm

    图 3  试验模型及加载方案

    Figure 3.  Test model and the loading method

    图 4  有限元模型

    Figure 4.  FE model of specimen

    图 5  测点位置

    Figure 5.  Position of measure points

    图 6  有限元模型与试验模型关键测点应力对比

    Figure 6.  Comparisons of tensile stresses of principal measure points in FE model and physical model

    图 7  关键测点主拉应力与作用循环次数间的关系

    Figure 7.  Principal stresses vs. loading cycles

    图 8  裂纹扩展路径对比

    Figure 8.  Comparisons of fatigue crack propagation paths

    图 9  试验模型装配式快速加固

    Figure 9.  Assembly reinforcement of test model

    图 10  裂纹尖端应变测点布置

    Figure 10.  Arrangement of test points on crack tip

    图 11  加固前后关键测点主拉应力与循环次数间的关系

    Figure 11.  Relationship between principal tensile stresses and loading cycles before and after strengthening

    图 12  加固前后裂尖应变与循环次数间的关系

    Figure 12.  Relationship between strain of crack tip and loading cycles before and after strengthening

    图 13  疲劳裂纹形状概貌

    Figure 13.  Fatigue crack shapes

    图 14  不同裂纹长度加固前后裂尖应力强度因子幅值

    Figure 14.  The stress intensity factors amplitude of the crack tips before and after the reinforcement in different crack lengths

    表  1  加固前后有效应力强度因子的变化

    Table  1.   Stress intensity factors before and after strengthening

    裂纹位置ΔKeff/(MPa•mm1/2降幅/%ΔKth/(MPa•mm1/2
    加固前加固后
    内侧裂纹495758563
    外侧裂纹522788563
    中裂纹324438763
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出版历程
  • 收稿日期:  2017-10-30
  • 修回日期:  2018-02-05
  • 网络出版日期:  2019-12-11
  • 刊出日期:  2020-02-01

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