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基于卷积神经网络双层壁三维热应力预测方法

黄俊杰 朱剑琴 程泽源

黄俊杰, 朱剑琴, 程泽源. 基于卷积神经网络双层壁三维热应力预测方法[J]. 航空动力学报, 2023, 38(7):1658-1667 doi: 10.13224/j.cnki.jasp.20220754
引用本文: 黄俊杰, 朱剑琴, 程泽源. 基于卷积神经网络双层壁三维热应力预测方法[J]. 航空动力学报, 2023, 38(7):1658-1667 doi: 10.13224/j.cnki.jasp.20220754
HUANG Junjie, ZHU Jianqin, CHENG Zeyuan. Three-dimensional thermal stress prediction method in double-wall structure using convolutional neural networks[J]. Journal of Aerospace Power, 2023, 38(7):1658-1667 doi: 10.13224/j.cnki.jasp.20220754
Citation: HUANG Junjie, ZHU Jianqin, CHENG Zeyuan. Three-dimensional thermal stress prediction method in double-wall structure using convolutional neural networks[J]. Journal of Aerospace Power, 2023, 38(7):1658-1667 doi: 10.13224/j.cnki.jasp.20220754

基于卷积神经网络双层壁三维热应力预测方法

doi: 10.13224/j.cnki.jasp.20220754
基金项目: 国家自然科学基金(51876005,52122604)
详细信息
    作者简介:

    黄俊杰(1998-),男,博士生,主要从事航空发动机涡轮叶片冷却结构寿命引导优化方法研究。E-mail:buaahjj@buaa.edu.cn

    通讯作者:

    程泽源(1992-),男,副研究员、硕士生导师,博士,主要从事人工智能技术在高效冷却系统设计中的应用等研究。E-mail:chengzeyuan@buaa.edu.cn

  • 中图分类号: V231.91

Three-dimensional thermal stress prediction method in double-wall structure using convolutional neural networks

  • 摘要:

    为实现三维物理场的预测,提出一种利用卷积神经网络(CNN)对双层壁冷却结构外壁三维热应力快速评估方法。针对双层壁冷却结构外壁平板状的结构特征,沿壁厚方向将温度场切分为多个切片。将温度作为卷积网络输入张量的基本元素,不同厚度位置的切片对应输入张量的通道维度,从而实现将三维温度场输入进网络,并输出在热载荷作用下的三维等效应力场。结果表明:训练收敛后的网络在测试集上的平均绝对误差为1.23 MPa,平均相对误差为15.10%,对峰值应力的平均绝对误差为16.10 MPa,平均相对误差为11.81%。对于双层壁冷却结构的热应力预测问题,CNN能够很好地完成温度到应力的映射。使用深度学习方法探究热弹性问题的潜在机理有望实现。

     

  • 图 1  技术路线图

    Figure 1.  Technology roadmap

    图 2  双层壁冷却结构单元

    Figure 2.  Double-wall cooling structural unit

    图 3  几何模型网格

    Figure 3.  Geometric model and mesh

    图 4  约束条件设置

    Figure 4.  Constraint setting

    图 5  有限元分析网格无关性检验

    Figure 5.  Grid independence check for finite element analysis

    图 6  数据处理示意图

    Figure 6.  Schematic diagram of data processing

    图 7  CNN网络结构

    Figure 7.  Architecture of the CNN

    图 8  训练集中ID1几何结构预测结果

    Figure 8.  Prediction results of ID1 geometry in the training set

    图 10  训练集和测试集上的绝对误差分布

    Figure 10.  Absolute error distribution on the training set and testing set

    图 9  测试集中ID1几何结构预测结果

    Figure 9.  Prediction results of ID1 geometry in the testing set

    图 11  训练集和测试集上预测应力场峰值应力回归分析

    Figure 11.  Peak stress regression analysis of predicted stress field on training set and testing set

    表  1  变量参数范围

    Table  1.   Range of variable parameters

    参数数值
    气膜孔直径Df /mm0.4~0.9
    气膜孔倾斜角α/(°)20~70
    气膜孔展向间距P/mm3Df~5Df
    气膜孔流向间距S/mm3Df~13Df
    外壁厚度Ho/mm0.7~1.2
    冲击距离H/mm0.7~1.2
    主流燃气温度Tm/K1 700, 1 900, 2 100
    主流燃气速度Vm/(m/s)400, 800
    吹风比M 0.75, 1.25
    下载: 导出CSV

    表  2  训练集和测试集各项指标结果

    Table  2.   Indexes results of the training set and testing set

    参数训练集测试集
    EMSE/MPa20.403.49
    EMAE/MPa0.431.23
    EMRE/%6.7515.10
    EPMAE/MPa2.6316.10
    EPMRE/%2.3911.81
    下载: 导出CSV

    表  3  样本各项变量的具体取值

    Table  3.   Values of each variable in the sample

    样本训练集样本
    ID1-CD1
    测试集样本
    ID1-CD7
    Df/mm0.85
    α/(°)30.16
    P/mm4.09Df
    S/mm12.84Df
    Ho/mm0.75
    Tm/K1700
    Vm/(m/s)400
    M0.751.25
    下载: 导出CSV
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出版历程
  • 收稿日期:  2022-09-30
  • 网络出版日期:  2023-05-11

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