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基于多尺度CNN和Transformer的航空发动机寿命预测方法

段佳俊 陆中 王捷

段佳俊, 陆中, 王捷. 基于多尺度CNN和Transformer的航空发动机寿命预测方法[J]. 航空动力学报, 2026, 41(3):20240311 doi: 10.13224/j.cnki.jasp.20240311
引用本文: 段佳俊, 陆中, 王捷. 基于多尺度CNN和Transformer的航空发动机寿命预测方法[J]. 航空动力学报, 2026, 41(3):20240311 doi: 10.13224/j.cnki.jasp.20240311
DUAN Jiajun, LU Zhong, WANG Jie. Aero-engine life prediction method based on multi-scale CNN and Transformer[J]. Journal of Aerospace Power, 2026, 41(3):20240311 doi: 10.13224/j.cnki.jasp.20240311
Citation: DUAN Jiajun, LU Zhong, WANG Jie. Aero-engine life prediction method based on multi-scale CNN and Transformer[J]. Journal of Aerospace Power, 2026, 41(3):20240311 doi: 10.13224/j.cnki.jasp.20240311

基于多尺度CNN和Transformer的航空发动机寿命预测方法

doi: 10.13224/j.cnki.jasp.20240311
基金项目: 国家重点研发计划(2023YFB4302403); 南京航空航天大学基本科研业务费国际科研合作伙伴培育基金(NG2023003); 南京航空航天大学科研与实践创新计划(xcxjh20230735)
详细信息
    作者简介:

    段佳俊(1999-),男,硕士,研究方向为航空发动机剩余寿命预测。E-mail:nostalgic_jj@nuaa.edu.cn

    通讯作者:

    陆中(1980-),男,教授,博士,研究方向为飞机系统安全性评估、系统可靠性工程。E-mail:luzhong@nuaa.edu.cn

  • 中图分类号: V240.2

Aero-engine life prediction method based on multi-scale CNN and Transformer

  • 摘要:

    目前在航空发动机剩余寿命预测中,通常仅考虑了单一尺度退化特征,并且在处理具有长期依赖关系的时序数据时效率低下。提出了一种基于多尺度CNN和Transformer的航空发动机剩余寿命预测方法。在传统CNN的基础上设计了多尺度特征提取模块,挖掘并融合了不同尺度下的退化特征;构造了特征连接模块,弥补了传统特征提取模块只能从同一层面提取特征的不足;基于Transformer的位置编码、多头自注意力机制和前馈神经网络实现了时序数据长期依赖特征的学习,利用多头注意力机制的并行计算能力降低了网络的运行时间。在C-MAPSS数据集上进行了实验验证,结果表明:所提方法与未提取多尺度特征的网络相比误差更小;并且相对于按顺序处理时序数据的RNN、LSTM和GRU等网络,运算时间分别降低了65.77%、48.41%和45.02%。

     

  • 图 1  模型训练过程

    Figure 1.  Flow chat of model training process

    图 2  多传感器的滑动时间窗口处理

    Figure 2.  Multi-sensor sliding time window processing

    图 3  MSCNNformer框架图

    Figure 3.  MSCNNformer framework diagram

    图 4  多尺度特征提取模块

    Figure 4.  Multi-scale feature extraction module

    图 5  多头注意力机制

    Figure 5.  Multi-head attention mechanism

    图 6  不同MFE与Encoder层数的结果

    Figure 6.  Results from different MFE & Encoder layers

    图 7  不同卷积核大小组合的结果

    Figure 7.  Results of different convolution kernel size combinations

    图 8  测试集的预测偏差分布(FD001~FD004)

    Figure 8.  Prediction deviation distribution of the test set (FD001—FD004)

    图 9  单台发动机的RUL预测结果(FD001~FD004)

    Figure 9.  RUL prediction for a single engine (FD001—FD004)

    表  1  预处理后的输入样本基本情况

    Table  1.   Preprocessed input sample details and labels

    数据集FD001FD002FD003FD004
    训练集中发动机数100260100249
    训练集中样本数17731488192182056518
    测试集中发动机数100259100248
    运行工况1616
    故障模式HPCHPCHPC&FANHPC&FAN
    输入时间窗尺寸30×920×1030×920×10
    下载: 导出CSV

    表  2  不同网络的训练时间

    Table  2.   Training time of different network

    方法 时间/s
    本文 1241.41
    RNN 3627.04
    LSTM 2257.98
    Bi-LSTM 2846.60
    GRU 2406.51
    Bi-GRU 2657.36
    下载: 导出CSV

    表  3  本文网络的最优参数

    Table  3.   Optimal parameters of the network

    参数 FD001 FD002 FD003 FD004
    最大周期数 100 100 100 100
    批大小 512 512 512 512
    窗口长度T 30 20 30 20
    L2正则化 0.001 0.001 0.0006 0.008
    Rearly 125 125 125 125
    dmodel 512 512 512 512
    头的数量 8 8 8 8
    学习率 0.0001 0.0001 0.0003 0.0001
    等待周期数 10 10 10 10
    激活函数 ReLU ReLU ReLU ReLU
    前馈层上的神经元数量 512/128 512/128 512/128 512/128
    下载: 导出CSV

    表  4  不同方法的RMSE对比

    Table  4.   RMSE comparison of different methods

    方法FD001FD002FD003FD004
    CNN[3]18.4530.2919.8229.16
    DCNN[4]12.6122.3612.6423.31
    HDNN[6]13.0215.2412.2218.16
    BLSTM-CNN[8]12.1316.0111.9618.10
    BiGRU-TSAM[10]12.5618.9412.4520.47
    MS-DCNN[11]11.4419.3511.6722.22
    MSTformer[15]14.4815.03
    MSFMTP[20]13.2414.8311.1714.09
    本文11.2613.6512.6313.53
    下载: 导出CSV

    表  5  不同方法的Score得分对比

    Table  5.   Score comparison of different methods

    方法FD001FD002FD003FD004
    CNN[3]12871357015967886
    DCNN[4]2731041228412466
    HDNN[6]24512822881527
    BLSTM-CNN[8]17412302421513
    BiGRU-TSAM[10]21322642333610
    MS-DCNN[11]19637472414844
    MSTformer[15]10991012
    MSFMTP[20]3405113119032817254290
    本文2511200724946
    下载: 导出CSV
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  • 收稿日期:  2024-05-15
  • 网络出版日期:  2025-12-26

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