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基于神经网络模型的一维特性预测算法优化

李洪宇 徐全勇 冯新龙

李洪宇, 徐全勇, 冯新龙. 基于神经网络模型的一维特性预测算法优化[J]. 航空动力学报, 2026, 41(4):20240420 doi: 10.13224/j.cnki.jasp.20240420
引用本文: 李洪宇, 徐全勇, 冯新龙. 基于神经网络模型的一维特性预测算法优化[J]. 航空动力学报, 2026, 41(4):20240420 doi: 10.13224/j.cnki.jasp.20240420
LI Hongyu, XU Quanyong, FENG Xinlong. Optimization of one-dimensional characteristic prediction algorithm based on neural network model[J]. Journal of Aerospace Power, 2026, 41(4):20240420 doi: 10.13224/j.cnki.jasp.20240420
Citation: LI Hongyu, XU Quanyong, FENG Xinlong. Optimization of one-dimensional characteristic prediction algorithm based on neural network model[J]. Journal of Aerospace Power, 2026, 41(4):20240420 doi: 10.13224/j.cnki.jasp.20240420

基于神经网络模型的一维特性预测算法优化

doi: 10.13224/j.cnki.jasp.20240420
基金项目: 国家科技重大专项(J2019-Ⅴ-0001-0092,J2019-Ⅴ-0013-0108); 清华大学自主科研计划(20234616001)
详细信息
    作者简介:

    李洪宇(2000-),男,硕士,主要从事科学计算与深度学习的工程应用研究。E-mail:842287615@qq.com

    通讯作者:

    徐全勇(1980-),男,副研究员,博士,主要从事航空发动机气动热力学方面的研究。E-mail:xuquanyong@tsinghua.edu.cn

  • 中图分类号: V231.3

Optimization of one-dimensional characteristic prediction algorithm based on neural network model

  • 摘要:

    基于CFD叶栅数据集构建了适用于多种叶型普遍工况的全连接神经网络落后角预测代理模型,对压气机特性预测HARIKA算法中的原有经验模型进行替换。通过拉丁超立方采样构建了涵盖NACA65、双圆弧、多圆弧三种主流叶型的58300组数据的数据集。对比全连接网络模型和支持向量机等8种机器学习回归模型基于NACA65叶型数据集的落后角预测学习能力,全连接模型落后角预测平均误差为0.06°,优于其他回归模型。在一维特性预测领域对多种叶型的落后角计算,使用不同叶型训练出的模型组合比多叶型数据训练出来的一个模型预测精度更高。在跨声速工况下与AI222-25型发动机两级风扇的实验数据对比,优化后HARIKA算法的压比特性预测相对误差平均下降9.06%,最高下降20.43%,证实该优化方法对提升HARIKA特性预测能力有一定帮助。

     

  • 图 1  不同升力系数和最大相对厚度的叶型几何[20]

    Figure 1.  Blade geometry with different lift coefficients and maximum relative thickness[20]

    图 2  双圆弧叶型

    Figure 2.  Double-circular-arc profile

    图 3  多圆弧叶型

    Figure 3.  Multi-circular-arc profile

    图 4  全连接神经网络

    Figure 4.  Full connect neural network

    图 5  LeakyReLU函数图像

    Figure 5.  Graph of LeakyReLU function

    图 6  机器学习模型预测结果

    Figure 6.  Machine learning model prediction results

    图 7  训练过程中的损失变化

    Figure 7.  Loss variation during training process

    图 8  全连接模型预测结果

    Figure 8.  Full connect model prediction results

    图 9  模型应用的两种方案

    Figure 9.  Two approaches for model application

    图 10  AI222-25二级风扇结构示意图

    Figure 10.  Schematic diagram of AI222-25 two-stage fans structure

    图 11  AI222-25二级风扇特性计算结果

    Figure 11.  Calculation results of AI22-25 two-stage fan characteristics

    表  1  数据集中各参数范围

    Table  1.   Range of parameters in the data set

    参数 取值范围
    NACA65 双圆弧 多圆弧
    攻角 −2~8 −5~8 −5~8
    进口马赫数 0.3~0.7 0.7~1.2 1.2~1.6
    叶型弯角 0~73 5~61 7~63
    稠度 0.5~2 1~2.5 1~2.2
    最大相对厚度 0.04~0.14 0.03~0.1 0.06~0.11
    前缘几何角 23~70 23~73 24~72
    下载: 导出CSV

    表  2  模型学习能力比较

    Table  2.   Comparison of model learning capabilities

    模型 评价指标
    LMSE LMAE R2
    线性回归 4.142 1.546 0.577
    决策树 0.662 0.364 0.939
    随机森林 0.141 0.107 0.973
    梯度提升 0.932 0.666 0.905
    支持向量机 0.596 0.344 0.942
    极端提升树 0.107 0.174 0.981
    多项式回归 2.006 0.336 0.814
    自适应增强 3.498 1.614 0.643
    下载: 导出CSV

    表  3  AI222-25二级风扇设计参数

    Table  3.   AI222-25 two-stage fan design parameters

    参数 设计值
    动叶 静叶
    转速/(r/min) 13200 0
    入口外径/mm 622, 604 613, 602
    出口外径/mm 613, 602 604, 600
    入口轮毂比 0.4305, 0.6798 0.5589, 0.6828
    出口轮毂比 0.5589, 0.6828 0.6298, 0.723
    叶片数 19, 29 42, 54
    稠度 1.61, 1.25 1.5, 1.39
    展弦比 1.244, 0.955 1.442, 1.147
    下载: 导出CSV

    表  4  模型在各转速工况特性预测误差

    Table  4.   Prediction error of model characteristics at different speed conditions

    折合转速 绝热效率$ \eta $ 总压比$ \pi $
    EMP FCNN EMP FCNN
    70 3.74 3.85 10.25 5.62
    80 4.04 4.45 12.91 0.94
    90 1.77 0.27 2.36 3.18
    100 2.94 1.38 35.29 14.86
    下载: 导出CSV
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  • 收稿日期:  2024-06-26
  • 网络出版日期:  2026-01-14

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