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多源融合的STFT-IncepNext航空发动机轴承故障诊断方法

万安平 张华 张今 蒋俊杰 王景霖 单添敏

万安平, 张华, 张今, 等. 多源融合的STFT-IncepNext航空发动机轴承故障诊断方法[J]. 航空动力学报, 2025, 40(10):20240049 doi: 10.13224/j.cnki.jasp.20240049
引用本文: 万安平, 张华, 张今, 等. 多源融合的STFT-IncepNext航空发动机轴承故障诊断方法[J]. 航空动力学报, 2025, 40(10):20240049 doi: 10.13224/j.cnki.jasp.20240049
WAN Anping, ZHANG Hua, ZHANG Jin, et al. Fault diagnosis of aeroengine bearings using multi-source fusion STFT-IncepNext method[J]. Journal of Aerospace Power, 2025, 40(10):20240049 doi: 10.13224/j.cnki.jasp.20240049
Citation: WAN Anping, ZHANG Hua, ZHANG Jin, et al. Fault diagnosis of aeroengine bearings using multi-source fusion STFT-IncepNext method[J]. Journal of Aerospace Power, 2025, 40(10):20240049 doi: 10.13224/j.cnki.jasp.20240049

多源融合的STFT-IncepNext航空发动机轴承故障诊断方法

doi: 10.13224/j.cnki.jasp.20240049
基金项目: 国家自然科学基金(52372420); 航空科学基金(20183333001)
详细信息
    作者简介:

    万安平(1983-),男,教授,博士,主要从事复杂装备健康管理及维修决策等研究。E-mail:wanap@zucc.edu.cn

    通讯作者:

    张今(1995-),男,博士生,主要从事高端装备流程挖掘、数字孪生技术等研究。E-mail:cicada@zju.edu.cn

  • 中图分类号: V263.6;TH133.33

Fault diagnosis of aeroengine bearings using multi-source fusion STFT-IncepNext method

  • 摘要:

    针对单传感器信息难以满足复杂工况下航空发动机轴承故障状态的稳定监测问题,提出一种STFT-IncepNext的航空发动机轴承故障诊断模型。首先,将同一时间窗口内的异位传感器数据进行拼接,以补充轴承在不同空间下的振动信息。其次,为了捕捉振动信号中故障成分的瞬时变化,利用短时傅里叶变换(short-time Fourier transform, STFT)将多传感器振动信号转换为时频图。最后,通过轻量化的IncepNext网络来提取时频图中蕴含的故障信息全局特征,由分类器给出识别的故障类别。实验结果表明:所提方法能够有效地增强信号的故障特征,提高轴承在不同状态下振动特征的辨识度。在特定的实验条件下,该方法实现了航空发动机轴承振动故障诊断准确率达100%,相较于STFT-EdgeNeXt、STFT-ResNeXt、STFT-ShuffleNet、STFT-ResNet18均取得了更好的性能,为航空发动机轴承故障诊断提供一种可行方法。

     

  • 图 1  STFT-IncepNext网络模型

    Figure 1.  Network model of STFT-IncepNext

    图 2  卷积编码器模块

    Figure 2.  Convolution encoder model

    图 3  SDTA编码器模块

    Figure 3.  SDTA encoder module

    图 4  多尺度分支卷积模块

    Figure 4.  Multi-scale branching convolution module

    图 5  直升机行星传动仿真实验平台

    Figure 5.  Helicopter planetary gearboxes transmission platform

    图 6  不同故障类型时频图

    Figure 6.  Time frequency diagram of different fault types

    图 7  STFT-IncepNext模型训练流程

    Figure 7.  STFT-IncepNext model training process

    图 8  不同传感器集合对模型准确率的影响

    Figure 8.  Influence of different sensor sets on model accuracy

    图 9  训练过程中损失函数和准确率

    Figure 9.  Loss function and accuracy during training process

    图 10  原始数据与分类层的特征可视化结果

    Figure 10.  Results of feature visualization of raw data and classification layer

    图 11  模型准确率差值

    Figure 11.  Model accuracy difference

    表  1  传感器布置点位

    Table  1.   Sensor placement points

    传感器类型采集仪对应位置安装位置
    转速NI_1驱动电动机输出轴
    加速度1NI_2(轴向)平行齿轮箱中间
    轴轴承端盖
    加速度2NI_3(水平径向)
    加速度3NI_4(垂直径向)
    加速度4NI_5平行齿轮箱右侧箱体
    (靠上轴承)
    加速度5NI_6承重台面(靠平行齿轮箱)
    下载: 导出CSV

    表  2  不同工况下的样本配置

    Table  2.   Sample configuration under different operating conditions

    工况编号 转频/Hz 负载/(N·m) 故障模式 样本量 样本点数
    1 34 22 5 200000 1000
    2 34 44 5 200000 1000
    3 57 22 5 200000 1000
    4 57 44 5 200000 1000
    下载: 导出CSV

    表  3  直升机传动系统实验台数据集

    Table  3.   Helicopter transmission system test bench dataset

    标签故障类型工况模式样本量
    0正常4800
    1滚动体4800
    2联合4800
    3内圈4800
    4外圈4800
    下载: 导出CSV

    表  4  不同诊断方法的准确率对比

    Table  4.   Comparison of accuracy between different diagnostic methods

    图像生成方法 模型方法 单传感器准确率/% 多传感器准确率/% 模型参数数量/106
    连续小波变换 CWT-IncepNext 79.83 87.50 1.46
    CWT-EdgeNeXt 73.44 84.55 1.16
    CWT-ResNet18 61.29 78.65 1.18
    CWT-ShuffleNet 70.63 73.96 1.26
    CWT-ResNeXt 70.49 86.11 22.99
    格拉姆角场 GAF-IncepNext 73.26 82.99 1.46
    GAF-EdgeNeXt 54.86 67.36 1.16
    GAF-ResNet18 63.37 78.99 1.18
    GAF-ShuffleNet 56.08 72.74 1.26
    GAF-ResNeXt 66.84 79.34 22.99
    短时傅里叶变换 STFT-IncepNext 98.33 100 1.46
    STFT-EdgeNeXt 98.17 99.83 1.16
    STFT-ResNet18 98.00 99.67 1.18
    STFT-ShuffleNet 78.83 91.33 1.26
    STFT-ResNeXt 97.50 99.83 22.99
    下载: 导出CSV
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  • 收稿日期:  2024-01-22
  • 网络出版日期:  2025-07-15

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