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Multiple cracks failure rule for TBM cutterhead based on three-dimensional crack propagation calculation

机译:基于三维裂纹传播计算的TBM切割机的多裂缝故障规则

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摘要

Practically, there is multiple cracks interpenetrating in TBM cutterhead, which gives rise to its failure prematurely. While the existing theoretical formulas and calculating methods cannot calculate its fatigue failure process under dynamic loading. In view of such situation, crack cutting sampling of TBM cutterhead after service and its fracture failure analysis were performed to clear that its fracture failure is mainly brittle fracture, based on which, A three-dimensional finite element crack propagation model was established to calculate the crack propagation process under dynamic loading. Stress intensity factor of compact test specimens is calculated by standard formula, and the growth paths of crack are got from multiple cracks fatigue tests, compared the two results obtained above to verify respectively the accuracy of the proposed method in calculating stress intensity factor and its growth path. It is confirmed that the two results about the change of stress intensity factor is basically match, and the maximum error of the growth path of the multiples crack model and the test result is about 3.7% within the permissible range. It is proved that the proposed method is feasible to calculate the multiple cracks failure process under the dynamic loading. Finally, the growth processes of collinear multiple cracks, parallel multiple cracks, nonparallel multiple cracks, and penetrating multiple cracks were calculated. The results show that the stress intensity factor at the intersection of collinear cracks decreased by about 26%, compared with a single crack. Parallel and non-parallel multiple cracks are attracted to each other as the cracks propagate in the process of growth and the stress intensity factor gradually decreases. Although the growth path and stress intensity factor do not change, the crack stops expanding, with the crack tip penetrates through another crack. The failure criterion of TBM cutterhead and the rule of interpenetration of multiple cracks proposed in this paper are the theoretical basis and technical support for the its life prediction and risk prediction.
机译:实际上,在TBM切割口中存在多个裂缝,这使其失效过早地产生。虽然现有的理论公式和计算方法无法在动态负载下计算其疲劳失效过程。鉴于这种情况,进行了裂缝切削术后的裂缝切削术及其断裂破坏分析,以清楚的是,其断裂衰竭主要是脆性骨折,基于该裂缝裂缝,建立了三维有限元裂纹传播模型来计算动态加载下的裂缝传播过程。通过标准式计算紧凑型试样的应力强度因子,并且从多个裂缝疲劳试验中获得裂缝的生长路径,比较上述两种结果分别验证了计算应力强度因子及其生长中提出的方法的准确性小路。证实,关于应力强度因子的变化的两个结果基本上匹配,并且倍数裂缝模型的生长路径的最大误差和测试结果在允许范围内约为3.7%。事实证明,该方法可行,可以在动态负载下计算多个裂缝故障过程。最后,计算了共线裂缝,平行多裂缝,非平行多裂缝和穿透多裂缝的生长过程。结果表明,与单一裂缝相比,共线裂缝交叉处的应力强度因子降低约26%。随着裂缝在生长过程中传播并且应力强度因子逐渐减小,平行和非平行多裂缝彼此吸引。虽然生长路径和应力强度因子不改变,但裂缝停止膨胀,裂缝尖端穿过另一个裂缝。本文提出的TBM切割机的故障标准和多个裂纹的互通的规则是其生命预测和风险预测的理论基础和技术支持。

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