地表堆载作用下盾构隧道结构响应机理与失效模式研究

Research on Structural Response Mechanism and Failure Mode of Shield Tunnels under Surface Surcharge Loading

  • 摘要: 为揭示淤泥质黏土地层中地表堆载对盾构隧道结构力学响应与失效机制的影响,通过开展1∶5物理模型试验,精细化模拟地层抗力、管片、螺栓及钢筋力学行为,并建立ABAQUS三环足尺有限元模型,系统分析不同堆载位置与埋深条件下的结构响应特征。结果表明:隧道收敛变形随荷载增加呈现弹性、变形发展、快速失稳、承载力退化及破坏五阶段演化过程;纵缝螺栓屈服形成塑性铰是控制结构整体破坏的关键,极限状态下4个塑性铰相继形成导致三次超静定体系失稳,结构最终呈现竖向压缩、水平扩张的“横鸭蛋”形破坏模式,竖向收敛变形达22.56%D。埋深由6.6 m增至19.8 m时,相同堆载下收敛变形降低约67%,截面最大弯矩降幅达49%;堆载偏心距增大会引起内力重分布,最大弯矩位置由拱顶偏移至拱肩,偏心距超过0.75D时可将变形控制在规范预警值以内。

     

    Abstract: To investigate the influence of surface surcharge on the structural mechanical response and failure mechanism of shield tunnels in soft clay strata, a 1∶5 physical model test was conducted to simulate the mechanical behaviors of stratum resistance, segments, bolts, and reinforcement in detail. A three-ring full-scale finite element model was established using ABAQUS to systematically analyze the structural response characteristics under different surcharge loading positions and burial depths. The results show that the tunnel convergence deformation exhibits a five-stage evolution process with increasing load, i.e., elasticity, deformation development, rapid instability, bearing capacity degredation, and failure. The formation of plastic hinges due to yielding of longitudinal joint bolts is critical to the overall failure of the structure. Under the ultimate state, the successive formation of four plastic hinges leads to the instability of the three-times statically indeterminate system, and the structure ultimately exhibits a "horizontal duck-egg" failure mode characterized by vertical compression and horizontal expansion, with vertical convergence deformation reaching 22.56% of the tunnel diameter. When the burial depth increases from 6.6 m to 19.8 m, the convergence deformation under the same surcharge load decreases by approximately 67%, and the maximum bending moment decreases by 49%. An increase in the eccentricity of the surface surcharge induces a redistribution of internal forces, shifting the locations of the maximum bending moments from the crown to the haunches. When the eccentricity exceeds 0.75 D, the deformations can be controlled within the allowable warning limits specified by the standards.

     

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