基于TPU材料层级结构的优化设计及吸能特性

李腾 张晨帆 邓庆田 李新波 温金鹏

李腾, 张晨帆, 邓庆田, 李新波, 温金鹏. 基于TPU材料层级结构的优化设计及吸能特性[J]. 高压物理学报, 2022, 36(6): 064104. doi: 10.11858/gywlxb.20220542
引用本文: 李腾, 张晨帆, 邓庆田, 李新波, 温金鹏. 基于TPU材料层级结构的优化设计及吸能特性[J]. 高压物理学报, 2022, 36(6): 064104. doi: 10.11858/gywlxb.20220542
LI Teng, ZHANG Chenfan, DENG Qingtian, LI Xinbo, WEN Jinpeng. Optimized Design and Energy Absorption of TPU Material Based on Hierarchical Structure[J]. Chinese Journal of High Pressure Physics, 2022, 36(6): 064104. doi: 10.11858/gywlxb.20220542
Citation: LI Teng, ZHANG Chenfan, DENG Qingtian, LI Xinbo, WEN Jinpeng. Optimized Design and Energy Absorption of TPU Material Based on Hierarchical Structure[J]. Chinese Journal of High Pressure Physics, 2022, 36(6): 064104. doi: 10.11858/gywlxb.20220542

基于TPU材料层级结构的优化设计及吸能特性

doi: 10.11858/gywlxb.20220542
基金项目: 国家自然科学基金委员会-中国工程物理研究院NSAF联合基金(U1930204)
详细信息
    作者简介:

    李 腾(1998-),男,硕士研究生,主要从事多孔材料与结构力学性能研究.E-mail:2020112046@chd.edu.cn

    通讯作者:

    邓庆田(1980-),男,博士,副教授,主要从事多孔材料与结构力学性能研究.E-mail:dengqt@chd.edu.cn

  • 中图分类号: O347

Optimized Design and Energy Absorption of TPU Material Based on Hierarchical Structure

  • 摘要: 选择柔性热塑性聚氨酯(TPU)为原料制备实验试样。基于面心立方层级结构,改变结构的直梁样式、间距,并将蜂窝结构层引入结构中,通过实验和有限元分析,研究层级结构在准静态加载下的变形模式和吸能特性。实验结果与有限元分析得到的载荷-位移曲线吻合较好。结果表明:与初始面心立方层级结构相比,增大直梁的振幅,调整直梁间距为2 mm,即增加塑性铰个数时,又或将蜂窝结构层引入层级结构,可以大幅提高层级结构的能量吸收性能;减小间距、增多塑性铰数目对改善层级结构吸能能力的效果最优;D-1构型与M-1构型相比,比吸能提高了46%;调整塑性铰位置时,层级结构会发生屈曲,不利于层级结构的能量吸收;与M-1构型相比,D-2和D-3构型的比吸能分别降低了27%和34%。

     

  • 图  面心立方层级结构(a)和不同振幅下的正弦曲线梁(b)

    Figure  1.  Face-centered cubic hierarchical structure (a) and sinusoidal beams of different amplitudes (b)

    图  调整直梁间距

    Figure  2.  Adjust the distance between straight beams

    图  蜂窝结构层:(a)正三角形,(b)内凹形

    Figure  3.  Honeycomb structure layer: (a) regular triangle,(b) re-entrant

    图  有限元模型

    Figure  4.  Finite element model

    图  不同网格尺寸下M-1构型的载荷-位移曲线(a)和能量时程曲线(b)

    Figure  5.  Force-displacement curves of M-1 with different mesh sizes (a) and time history of energy (b)

    图  实验试样 (a) 和CMT5305万能试验机 (b)

    Figure  6.  Experimental samples (a) and CMT5305 universal testing machine (b)

    图  (a) 拉伸试样及尺寸和 (b) TPU材料的应力-应变曲线

    Figure  7.  (a) Tensile specimens and its dimensions,(b) stress-strain curve of TPU

    图  调整幅值(a)、间距(b)、角度(c)以及插入蜂窝结构层(d)时层级结构试样的载荷-位移曲线

    Figure  8.  Force-displacement curves of hierarchical structure sample: adjustment of (a) amplitude, (b) distance, (c) angle and (d) introducing honeycomb structural layers

    图  M-1试样不同阶段变形模式的实验与有限元模拟结果对比

    Figure  9.  Experimental and finite element simulation comparison of deformation modes of M-1 specimens at different stages

    图  10  M-1试样的实验与有限元模拟载荷-位移曲线对比

    Figure  10.  Comparison of experimental and finite element simulation of force-displacement curves for M-1 specimens

    图  11  不同振幅层级结构在不同应变下的变形

    Figure  11.  Deformation of hierarchical structures of different amplitude under various strains

    图  12  不同振幅层级结构的EASEA

    Figure  12.  EA and SEA of hierarchical structure ofdifferent amplitudes

    图  13  不同间距层级结构在不同应变下的变形

    Figure  13.  Deformation of hierarchical structures of different distance under various strains

    图  14  不同间距层级结构的EASEA

    Figure  14.  EA and SEA of hierarchical structure ofdifferent distance

    图  15  不同角度层级结构在不同应变下的变形

    Figure  15.  Deformation of hierarchical structures of different angle under various strains

    图  16  不同角度层级结构的EASEA

    Figure  16.  EA and SEA of hierarchical structure ofdifferent straight beam angles

    图  17  不同应变下蜂窝层级结构的变形情况

    Figure  17.  Deformation of honeycomb hierarchical structures under various strains

    图  18  蜂窝层级结构的EASEA

    Figure  18.  EA and SEA of hierarchical structure with honeycomb structure layer

    表  1  4种设计方法获得的几何模型的具体结构特征

    Table  1.   Specific structural features of geometric models obtained by four design methods

    ModelSpecific structural features
    Distance/mmAmplitude/mmAngle/(º)
    M-1300, 90
    AM-130.250, 90
    AM-230.500, 90
    AM-331.000, 90
    D-1200, 90
    D-22-4-200, 90
    D-34-2-400, 90
    AN-100, 45
    AN-200, 45, 135
    AN-300, 90, 45, 135
    AN-400, 30, 60, 90
    H-1Honeycomb structure layer: equilateral triangle
    H-2Honeycomb structure layer: re-entrant
    下载: 导出CSV

    表  2  打印试样的质量

    Table  2.   Mass of the 3D printed sample

    ModelMass/g ModelMass/g
    M-16.92 AN-19.01
    AM-17.63AN-28.72
    AM-27.74AN-38.38
    AM-39.39AN-47.73
    D-19.26H-110.05
    D-26.66H-29.15
    D-36.71
    下载: 导出CSV
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出版历程
  • 收稿日期:  2022-03-21
  • 修回日期:  2022-04-07
  • 录用日期:  2022-04-20
  • 刊出日期:  2022-12-05

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