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基于机器学习的新型多胞梯度结构设计与优化

闫凯波 周鹏 陆思思 王俊杰 范志伟

闫凯波, 周鹏, 陆思思, 王俊杰, 范志伟. 基于机器学习的新型多胞梯度结构设计与优化[J]. 爆炸与冲击. doi: 10.11883/bzycj-2025-0388
引用本文: 闫凯波, 周鹏, 陆思思, 王俊杰, 范志伟. 基于机器学习的新型多胞梯度结构设计与优化[J]. 爆炸与冲击. doi: 10.11883/bzycj-2025-0388
YAN Kaibo, ZHOU Peng, LU Sisi, WANG Junjie, FAN Zhiwei. Design and Optimization of Corrugated Multi-cell Gradient Structures Based on Machine Learning[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2025-0388
Citation: YAN Kaibo, ZHOU Peng, LU Sisi, WANG Junjie, FAN Zhiwei. Design and Optimization of Corrugated Multi-cell Gradient Structures Based on Machine Learning[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2025-0388

基于机器学习的新型多胞梯度结构设计与优化

doi: 10.11883/bzycj-2025-0388
基金项目: 国家自然科学基金(52402466);中国博土后科学基金(2022M723001, 2022M713014);重庆市自然科学基金(CSTB2025NSCQ-GPX0885);重庆市技术创新与应用发展专项重点项目(CSTB2024TIAD-KPX0081);重庆市博土后研究项目(2022CQBSHTB2020);重庆市教育委员会科学技术研究项目(KJZD-K202400704, KJQN202400718);重庆交通大学研究生科研创新项目(2025S0051)
详细信息
    作者简介:

    闫凯波(1992- ),男,博士,讲师,kaibo_yan@yeah.net

    通讯作者:

    陆思思(1993- ),女,博士,副教授,sisi_lu2020@yeah.net

  • 中图分类号: O342

Design and Optimization of Corrugated Multi-cell Gradient Structures Based on Machine Learning

  • 摘要: 针对航空航天、交通运输、土木建筑等领域的碰撞防护需求,提出一种新型多胞梯度结构管(CMGHT)设计方法:在普通六边形管内引入正弦波纹肋板,并融合功能梯度设计理念,以实现结构耐撞性能的提升。首先,构建该结构的有限元模型并开展数值模拟分析。结果显示,在相同壁厚条件下,CMGHT的关键吸能指标表现显著优于现有结构,相较于普通六边形管(HT),其吸收能量(Ea)、比吸能(Esa)、平均压缩力($ \overline{F} $)及压缩效率(η)分别提升390%、76%、395%和46%;相较于多胞六边形管(MHT),上述指标分别提升121%、58%、121%和97%;相较于波纹多胞六边形管(CMHT),EaEsa、$ \overline{F} $、η分别提升7%、7%、8%、33%,且初始峰值压缩力(Fmax)降低18%,充分证明其吸能性能更优。随后,以肋板与外管的几何参数为设计变量,通过全因子试验设计生成540组样本,构建支持向量机(SVM)代理模型,并结合冠豪猪优化(CPO)算法完成模型优选,实现对CMGHT耐撞性能的精准预测。最后,采用多目标浣熊优化算法(MOCOA)进行多目标优化,获取最优特征参数组合。优化结果表明,相较于未经过参数优化的CMGHT基础模型(参数基于工程常用范围初步设定:肋板厚度1 mm、肋板幅值3 mm、外管梯度厚度0.5 mm-1 mm-1.5 mm、外管长度33.3 mm),优化后结构的Esa提高22%,η提升53%,$ \overline{F} $增强270%,进一步验证了设计方法的有效性。
  • 图  1  CMGHT的构建过程

    Figure  1.  The construction process of CMGHT

    图  2  CMGHT的有限元模型

    Figure  2.  FE model of CMGHT

    图  3  HT的变形模式与压缩曲线对比

    Figure  3.  Comparison of the deformation mode and compression curve of HT

    图  4  各结构管力-位移曲线图

    Figure  4.  The force-displacement curves of the various structural tubes.

    图  5  不同结构管的耐撞性指标雷达图

    Figure  5.  The radar chart of crashworthiness indicators for various structural tubes.

    图  6  不同结构管的压缩变形

    Figure  6.  Compressive deformation of different structural tubes

    图  7  测试集的预测结果对比

    Figure  7.  Comparison of prediction results for test set

    图  8  MOCOA流程

    Figure  8.  Flowchart of MOCOA.

    图  9  帕累托前沿解

    Figure  9.  The Pareto front solutions.

    图  10  帕累托解集的平面投影

    Figure  10.  Plane projection of Pareto solution set.

    图  11  解B有限元仿真力-位移曲线

    Figure  11.  The force-displacement curve of FE simulation for Solution B

    图  12  优化后CMGHT压缩变形

    Figure  12.  The deformation sequence of the optimized CMGHT

    表  1  HT的耐撞性指标对比

    Table  1.   Comparison of the crashworthiness indicators of HT

    方法Fmax/kNEa/kJ$ \overline{F} $/kNη/%Esa/(J·g−1)
    FE20.780.819.64466.982
    QS[23]20.380.829.78477.086
    误差1.9%1.3%1.4%2.1%1.4%
    下载: 导出CSV

    表  2  不同结构管的耐撞性指标对比

    Table  2.   Comparison of the crashworthiness indicators of different structural tubes

    结构 Fmax/kN Ea/kJ $ \overline{F} $/kN $ \eta $/% Esa/(J·g−1)
    HT 18.18 0.51 7.22 39 6.25
    MHT 55.28 1.13 16.20 29 6.96
    CMHT 76.20 2.33 33.25 43 10.26
    CMGHT 62.27 2.50 35.75 57 10.97
    下载: 导出CSV

    表  3  CMGHT参数取值范围

    Table  3.   Design parameter ranges for CMGHT

    参数 tr/mm A/mm t0/mm D/mm
    取值范围 0.5~3 1~3 0.5~5 33.3~70
    下载: 导出CSV

    表  4  不同优化算法模型收敛性能对比[31-33]

    Table  4.   Comparison of convergence performance for different optimization algorithm models[3133]

    优化算法平均收敛代数适应度
    遗传算法(GA)32±80.142 00
    粒子群算法(PSO)18±50.121 00
    CPO6±30.019 89
    下载: 导出CSV

    表  5  SVM与CPO-SVR模型的超参数

    Table  5.   Hyperparameters of SVM and CPO-SVR models

    核心参数SVMCPO-SVR搜寻范围
    核参数1.08.1449[0.1,100]
    惩罚因子0.250.9322[0.01,10]
    下载: 导出CSV

    表  6  参数取值边界处与参数范围外CMGHT预测性能

    Table  6.   CMGHT prediction performance at the parameter boundary and beyond the parameter range

    结构参数Esa/(J·g−1)误差Fmax/kN误差$ \overline{F} $/kN误差
    3.2-3-4.1-72(仿真)18.127.4%251.895.2%208.546.6%
    3.2-3-4.1-72(预测)16.77238.73194.71
    3.4-3-1-30(仿真)13.411.8%181.165.9%110.415.2%
    3.4-3-1-30(预测)13.16170.44116.20
    0.5-1-1-30(仿真)6.782.3%31.179.2%12.676.5%
    0.5-1-1-30(预测)6.6234.0513.5
    3.1-1-4.3-74(仿真)15.094.9%211.027.2%154.71.9%
    3.1-1-4.3-74(预测)14.34195.82151.71
    3-1-0.9-30(仿真)9.993.2%113.016.5%53.814.9%
    3-1-0.9-30(预测)9.67105.6056.49
    3-3-4.2-70(仿真)16.363.4%244.920.4%193.253.6%
    3-3-4.2-70(预测)15.81246.14186.11
    3-1-1-30(仿真)10.389.7%117.854.2%57.452.2%
    3-1-1-30(预测)11.39122.8856.14
    3-3-5-70(仿真)16.170.3%238.620.4%187.20.5%
    3-3-5-70(预测)16.12237.59186.2
    下载: 导出CSV

    表  7  COA与PSO和GA的对比[37]

    Table  7.   Comparison of COA, PSO, and GA[37]

    对比维度 COA PSO GA
    CEC-2017(维度为10)核心函数表现 C1(单模态):均值为100,标准差为1.33·10−5
    C3(单模态):均值为300,标准差为4.64·10−14
    C10(多模态):均值为1270.97,标准差为112.83
    C1:均值为3347.23,标准差为4427.81
    C3:均值为329.38,标准差为8.604
    C10:均值为2013.59,标准差为348.99
    C1:均值为12641048,标准差为4849091
    C3:均值为15733.23,标准差为10584.32
    C10:均值为1766.65,标准差为320.45
    CEC-2017(维度为100)核心函数表现 C4(多模态):均值为770.53,标准差为51.36
    C6(复合函数):均值为636.39,标准差为2.37
    C8(复合函数):均值为1393.98,标准差为128.98
    C4:均值为2592.37,标准差为746.46
    C6:均值为663.56,标准差为6.46
    C8:均值为1733.68,标准差为66.67
    C4:均值为9756.10,标准差为535.13
    C6:均值为665.26,标准差为6.76
    C8:均值为2070.20,标准差为45.98
    CEC-2011(实际问题)表现 C11-F1:均值为2.84,标准差为5.69
    C11-F7:均值为0.75,标准差为0.12
    C11-F12:均值为1186100,标准差为42666.96
    C11-F1:均值为19.48,标准差为6.94
    C11-F7:均值为1.15,标准差为0.32
    C11-F12:均值为2428911,标准差为176214.5
    C11-F1:均值为25.59,标准差为1.27
    C11-F7:均值为1.83,标准差为0.28
    C11-F12:均值为15862796,标准差为113798.6
    收敛速度(CEC-2017 维度为30) 迭代500步时,C10函数均值为4032.98
    接近全局最优;收敛曲线陡峭
    迭代500步时,C10函数均值为228.98,
    仅达到COA的81.3%;前期探索缓慢
    迭代500步时,C10函数均值为6407.28,仅达到COA的62.9%;后期收敛停滞
    下载: 导出CSV

    表  8  三个帕累托最优解的结构参数

    Table  8.   Structural parameters of three Pareto optimal solutions

    tr/mm A/mm t0/mm D/mm
    A 3 3 1.5-2.2-2.4 65
    B 2.5 3 0.9-2.2-5 48
    C 3 3 0.5-1.8-4.1 44
    下载: 导出CSV

    表  9  三种帕累托最优解的对比

    Table  9.   Comparison of the three Pareto optimal solutions

    Esa/(J·g−1)Fmax/kN$ \overline{F} $/kNη/%
    A12.35118.9296.380
    B13.06146.03129.188
    C12.86187.11156.283
    下载: 导出CSV

    表  10  模拟结果与预测结果的对比

    Table  10.   Comparison of the simulation and prediction results

    Esa/(J·g−1)Fmax/kN$ \overline{F} $/kN
    预测13.06146.03129.1
    仿真13.33150.81132.1
    误差2%3.1%2.2%
    下载: 导出CSV

    表  11  CMGHT优化前后各组件吸能对比

    Table  11.   Comparison of energy absorption of each component before and after CMGHT optimization

    对照组外管吸能/kJ占比/%肋板吸能/kJ占比/%外管-肋板相互作用耗能/kJ占比/%Ea/kJ
    优化前0.5923.61.8720.114.42.5
    优化后3.2535.15.6160.70.394.29.25
    下载: 导出CSV

    表  12  CMGHT基础模型与优化后CMGHT的耐撞性能对比

    Table  12.   Comparison of the crashworthiness performance of original CMGHT and optimized CMGHT

    对照组Esa/(J·g−1)η/%$ \overline{F} $/kN
    优化前10.9657.4135.7
    优化后13.3387.59132.1
    下载: 导出CSV
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