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钢桥面板典型焊接构造细节疲劳裂纹扩展数值模拟

Numerical simulation of fatigue crack propagation of typical welded structural details in steel bridge decks

  • 摘要: 为研究钢桥面板典型构造细节在焊接残余应力与车辆荷载耦合作用下疲劳开裂问题,对U肋双面焊连接部位、U肋-横隔板连接部位进行焊接过程数值模拟,建立钢桥面板壳−实体单元耦合的节段有限元模型,基于扩展有限元法进行静态应力强度因子计算和动态裂纹扩展行为分析.研究结果表明,U肋双面焊连接部位和U肋-横隔板连接部位焊缝区域均存在较大的焊接残余拉应力,其最大值均接近钢材的屈服强度;在仅考虑车辆荷载作用下,U肋双面焊节点的顶板内、外侧焊趾处的疲劳裂纹以及U肋-横隔板构造细节的横隔板弧形开孔处均不会开裂;U肋腹板焊趾处和横隔板焊趾处会发生开裂,但与实桥扩展情况不一致;引入焊接残余应力后,顶板内侧焊趾处的裂纹比外侧焊趾处裂纹扩展更快,裂纹类型均为以Ⅰ型主导的Ⅰ-Ⅱ-Ⅲ型复合裂纹;U肋腹板焊趾处裂纹是以Ⅰ型为主导的Ⅰ-Ⅱ-Ⅲ型复合裂纹,横隔板焊趾处的疲劳裂纹是以Ⅰ型为主导的Ⅰ-Ⅱ型复合裂纹;横隔板弧形开孔处属于Ⅰ型开裂.

     

    Abstract: In order to investigate the fatigue cracking of typical structural details of steel bridge decks under the coupling of welding residual stress and vehicle loads, a numerical simulation of the welding process was carried out for the U-rib double-sided welded joints and U-rib–diaphragm joints, and a shell-solid coupled segmented finite element model for steel bridge decks was established to carry out the calculation of the static stress intensity factor and the analysis of the dynamic crack propagation behavior based on the extended finite element method (XFEM). The results show that high welding residual tensile stresses can be observed in the weld area of the U-rib double-sided welded joints and the U-rib–diaphragm joints, with maximum values close to the yield strength of the steel. By considering only the vehicle load, fatigue cracks in the roof and the weld toe of the U-rib double-sided welded joints will not propagate, as well as those in the arc-shaped openings on the diaphragm of the U-rib structure. However, fatigue cracks in the weld toe of the U-rib web and the diaphragm will propagate, but do not consistent with actual bridge observations. After introducing welding residual stress, the crack at the inner weld toe of the roof propagates faster than at the outer weld toe, and it becomes mixed cracks of ModeⅠ–Ⅲ, led by Mode Ⅰ; the crack in U-rib web weld toe is mixed cracks of Mode Ⅰ–Ⅱ–Ⅲ, led by Mode Ⅰ; the fatigue crack in diaphragm weld toe is mixed cracks of Mode Ⅰ–Ⅱ, led by Mode Ⅰ. The fatigue crack in the arc-shaped openings on the diaphragm is Mode Ⅰ.

     

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