基于应变模态的受电弓上框架肘接裂纹损伤识别

Crack Damage Identification of Pantograph Upper Frame Elbow Joint Based on Strain Mode

  • 摘要:
    目的 受电弓结构安全对列车运行的可靠性有重要影响。列车受电弓肘接位置易出现疲劳裂纹现象。对此,有必要利用其振动特性,准确识别裂纹萌生前期的、不易被发现的微小裂纹损伤,并分析其特性。
    方法 介绍了基于应变模态的损伤识别理论,以某型受电弓上框架为研究对象建立有限元模型进行模态仿真计算,通过实体模态试验验证了模态频率仿真结果的准确性,计算分析了受电弓上框架位移模态和应变模态振型。选取前2阶应变模态,以应变模态变化率均值作为损伤指标来识别裂纹。计算了不同裂纹尺寸对应变模态的影响。
    结果及结论 裂纹的产生不会对其振型和频率产生较大影响。应变模态在裂纹位置处会产生明显突变,而位移模态不会产生变化。应变模态比位移模态对损伤更敏感,上框架应变模态会在裂纹损伤位置处产生突变,低阶次效果最为明显,高阶次损伤带来的变化可能会被隐藏。随着裂纹尺寸的增大,应变模态在裂纹位置处产生的突变越大。损伤指标值随着裂纹深度的增大而增大;裂纹长度小于10.00 mm时,损伤指标值差别较小,裂纹长度大于10.00 mm时,损伤指标值随着裂纹长度的增大而增大。

     

    Abstract:
    Objective The structural safety of pantograph has a significant impact on the operational reliability of trains. Fatigue cracks are prone to occur at the elbow joints of pantograph on high-speed trains. Therefore, it is necessary to utilize their vibration characteristics to accurately identify the hardly detectable small cracks in their early-stage initiation and to analyze their characteristics.
    Method The damage identification theory based on strain mode is introduced. Taking the upper frame of a certain type of pantograph as the research object, a finite element model is established to perform modal simulation analysis. The accuracy of the simulated modal frequency results is verified through a physical modal test. The displacement mode and strain mode shapes of the pantograph upper frame are calculated and analyzed. The first two strain mode orders are selected, and the mean value of the strain mode change rate is adopted as the damage index to identify cracks. The influence of different crack sizes correspond to strain modes is calculated.
    Result & Conclusion  The occurrence of cracks has no significant effect on mode shape or frequency. At the crack location, the strain mode exhibits a pronounced mutation, whereas the displacement mode does not change. The strain mode is more sensitive to damage than the displacement mode. The strain mode of upper frame shows a distinct mutation at the crack damage location, with the effect being most evident in the lower-order modes, while the changes caused by higher-order mode damage may be concealed. As the crack size increases, the mutation of the strain mode at the crack location becomes more significant. The damage index value increases with the increase in crack depth; when the crack length is less than 10.00 mm, the difference in damage index value is small, and when the crack length exceeds 10.00 mm, the damage index value will increase with the crack length.

     

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