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带襟翼导轨翼肋后缘尺寸-拓扑综合优化的摄动神经网络代理模型法

谢川 徐超 周丹发 姚卫星

谢川, 徐超, 周丹发, 姚卫星. 带襟翼导轨翼肋后缘尺寸-拓扑综合优化的摄动神经网络代理模型法[J]. 应用数学和力学, 2024, 45(1): 61-71. doi: 10.21656/1000-0887.440033
引用本文: 谢川, 徐超, 周丹发, 姚卫星. 带襟翼导轨翼肋后缘尺寸-拓扑综合优化的摄动神经网络代理模型法[J]. 应用数学和力学, 2024, 45(1): 61-71. doi: 10.21656/1000-0887.440033
XIE Chuan, XU Chao, ZHOU Danfa, YAO Weixing. The Perturbation Neural Network Surrogate Model Method for Size-Topology Synthetical Optimization of Wing Rib Trailing Edges With Flap Tracks[J]. Applied Mathematics and Mechanics, 2024, 45(1): 61-71. doi: 10.21656/1000-0887.440033
Citation: XIE Chuan, XU Chao, ZHOU Danfa, YAO Weixing. The Perturbation Neural Network Surrogate Model Method for Size-Topology Synthetical Optimization of Wing Rib Trailing Edges With Flap Tracks[J]. Applied Mathematics and Mechanics, 2024, 45(1): 61-71. doi: 10.21656/1000-0887.440033

带襟翼导轨翼肋后缘尺寸-拓扑综合优化的摄动神经网络代理模型法

doi: 10.21656/1000-0887.440033
详细信息
    作者简介:

    谢川(1992—),男,博士生(E-mail: xcshovelm@nuaa.edu.cn)

    通讯作者:

    姚卫星(1957—),男,教授,博士,博士生导师(通讯作者. E-mail: wxyao@nuaa.edu.cn)

  • 中图分类号: O342

The Perturbation Neural Network Surrogate Model Method for Size-Topology Synthetical Optimization of Wing Rib Trailing Edges With Flap Tracks

  • 摘要: 带襟翼导轨的翼肋后缘设计需要确定肋缘条、腹板的尺寸和肋腹板的拓扑形状,对此提出了一种针对尺寸-拓扑综合优化的摄动神经网络(perturbation neural network, PNN)代理模型法. 其基本思想是基于拓扑优化对参数的敏感性,引入了对试验设计(design of experiments, DOE)样本点的摄动,通过过滤手段捕获拓扑突变点,并降低数值噪声,极大地提高了代理模型的预测精度,将拓扑优化过程作为黑盒,直接建立起尺寸变量与拓扑优化后结构响应的代理模型. 最后在代理模型上进行优化,得到了结构尺寸与拓扑形状的最优组合. 该文完成了一个翼肋后缘优化典型算例,证明了该方法的有效性和优越性.
  • 图  1  带襟翼导轨的翼肋后缘结构初始模型

    Figure  1.  The initial model for the trailing edge of the wing rib with a flap track

    图  2  翼肋后缘结构基本尺寸与变量定义

      为了解释图中的颜色,读者可以参考本文的电子网页版本,后同.

    Figure  2.  Dimensions of trailing edge of wing rib structure and definition of design variables

    图  3  ANN与PNN构成对比

    Figure  3.  Comparison between ANN and PNN

    图  4  优化流程

    Figure  4.  Optimization flow chart

    图  5  尺寸优化后模型应力分布

    Figure  5.  Model stress distributions after size optimization

    图  6  翼肋形状设计过程

    Figure  6.  The wing rib shape design process

    图  7  拓扑重量关于尺寸变量的归一化灵敏度箱型图

    Figure  7.  The normalized sensitivity box diagram of the topological weight with respect to size variables

    图  8  基于PNN的尺寸-拓扑综合优化结果

    Figure  8.  Results of the size-topology synthetical optimization based on PNN

    表  1  代理模型预测精度及特点[21]

    Table  1.   Prediction accuracy and characteristics of the surrogate model[21]

    surrogate model prediction accuracy characteristic
    PRS low high efficiency
    Kriging high sensitivity to digital noise
    RBF medium the best effect in general
    下载: 导出CSV

    表  2  变量说明及取值范围

    Table  2.   Variable description and range

    variable name symbol range
    upper edge strip thickness t1/mm 3.0~8.0
    middle edge strip thickness t2/mm 3.0~8.0
    lower edge strip thickness t3/mm 3.0~8.0
    lower web thickness t4/mm 3.0~8.0
    upper web thickness t5/mm 1.0~4.0
    下载: 导出CSV

    表  3  传统优化中变量与响应各阶段结果

    Table  3.   Variable and response results at each stage in traditional optimization

    variable or response initial value 1st size optimization final result
    t1/mm 3.00 3.26 3.00
    t2/mm 3.00 3.00 3.00
    t3/mm 3.00 3.00 3.00
    t4/mm 3.00 3.70 4.54
    t5/mm 1.00 1.49 1.56
    δmax/mm 10.72 9.57 10.90
    σmax/MPa 394.60 299.99 299.94
    w/kg 1.842 2.12 2.06
    下载: 导出CSV

    表  4  基于PNN的优化结果

    Table  4.   Optimization results based on PNN

    variable or response t1/mm t2/mm t3/mm t4/mm t5/mm δ/mm σ/MPa w/kg
    result 3.00 3.00 3.00 3.71 1.72 7.44 300.15 1.90
    下载: 导出CSV

    表  5  代理模型精度对比

    Table  5.   Surrogate model accuracy comparison

    criterion Kriging with PNN PRS with PNN RBF with PNN Kriging without PNN
    R2 0.915 0.536 0.897 0.782
    RRMSE 0.105 0.254 0.112 0.197
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-02-13
  • 修回日期:  2023-03-15
  • 刊出日期:  2024-01-01

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