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基于FDG-YOLO轻量化模型的航空发动机损伤检测方法

蔡舒妤 何冲

蔡舒妤,何冲. 基于FDG-YOLO轻量化模型的航空发动机损伤检测方法[J]. 北京航空航天大学学报,2026,52(4):1055-1063
引用本文: 蔡舒妤,何冲. 基于FDG-YOLO轻量化模型的航空发动机损伤检测方法[J]. 北京航空航天大学学报,2026,52(4):1055-1063
CAI S Y,HE C. Damage detection method for aero-engine based on FDG-YOLO lightweight model[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(4):1055-1063 (in Chinese)
Citation: CAI S Y,HE C. Damage detection method for aero-engine based on FDG-YOLO lightweight model[J]. Journal of Beijing University of Aeronautics and Astronautics,2026,52(4):1055-1063 (in Chinese)

基于FDG-YOLO轻量化模型的航空发动机损伤检测方法

doi: 10.13700/j.bh.1001-5965.2024.0024
基金项目: 

中央高校基本科研业务费专项资金(3122023PY11);复杂零部件智能检测与识别湖北省工程研究中心开放课题资助(IDICP-KF-2024-07)

详细信息
    通讯作者:

    E-mail:csy0313@163.com

  • 中图分类号: V263.6;TP391.41

Damage detection method for aero-engine based on FDG-YOLO lightweight model

Funds: 

The Fundamental Research Funds for the Central Universities (3122023PY11); Open Projects funded by Hubei Engineering Research Center for Intelligent Detection and Identification of Complex Parts (IDICP-KF-2024-07)

More Information
  • 摘要:

    针对航空发动机损伤检测深度学习模型在嵌入式设备上部署应用的实时性差、检测精度低等问题,提出一种轻量化航空发动机损伤检测模型FDG-YOLO。引入FasterNet网络重构YOLOv5的主干网络,解决主干网络参数量大的问题;通过深度可分离卷积改进YOLOv5颈部网络的普通卷积,减少颈部网络的冗余参数;以GSConv为基础构建GS C3结构,替换原模型的C3结构,增强模型的表达能力和感受野;在航空发动机损伤数据集进行实验验证。结果表明:与YOLOv5原模型相比,所提FDG-YOLO模型参数量降低了52.5%,浮点运算速度降低了66%,在嵌入式设备上的平均精度均值(mAP)达到89.6%,高于其他轻量化模型,帧率达到61帧/s,检测速度适配于发动机损伤图像采集速度,能够更好地满足航空发动机损伤检测的智能化应用需求。

     

  • 图 1  FDG-YOLO轻量化航空发动机损伤检测模型

    Figure 1.  FDG-YOLO lightweight aero-engine damage detection model

    图 2  基于FasterNet的损伤检测模型主干网络改进

    Figure 2.  Improvement of backbone network of damage detection model based on FasterNet

    图 3  普通卷积与深度可分离卷积

    Figure 3.  Ordinary convolution and depthwise separable convolution

    图 4  基于DSConv的损伤检测模型CBS结构改进

    Figure 4.  Improvement of CBS structure in damage detection model based on DSConv

    图 5  GSConv结构

    Figure 5.  GSConv structure

    图 6  C3结构和GS C3结构

    Figure 6.  C3 structure and GS C3 structure

    图 7  基于FDG-YOLO轻量化模型的航空发动机损伤检测方法流程

    Figure 7.  Workflow of aero-engine damage detection method based on FDG-YOLO lightweight model

    图 8  航空发动机损伤图像

    Figure 8.  Aero-engine damage images

    图 9  不同模型检测结果对比

    Figure 9.  Comparison of detection results of different models

    表  1  数据集样本分布

    Table  1.   Sample distribution of dataset

    损伤类型 训练集 验证集 测试集
    烧蚀 1360 343 125
    凹痕 857 140 85
    裂纹 827 136 85
    材料缺失 1756 581 150
    下载: 导出CSV

    表  2  消融实验结果

    Table  2.   Ablation experimental results

    模型 参数量 mAP/% 浮点运算速度/109 s−1 帧率/(帧·s−1)
    实验a 20 865 057 92.0 47.9 92
    实验b 11 654 613 88.3 22.5 139
    实验c 9 633 429 88.1 20.0 150
    实验d 9 909 621 90.5 16.3 142
    下载: 导出CSV

    表  3  不同模型检测性能对比

    Table  3.   Comparison of detection performance of different models

    模型 参数量 mAP/% 浮点运算速度/109 s−1 帧率/(帧·s−1)
    YOLOv3-tiny 8 673 622 86.7 12.9 159
    YOLOv7-tiny 6 014 737 89.5 13.0 63
    FDG-YOLO 9 909 621 90.5 16.3 142
    下载: 导出CSV

    表  4  嵌入式设备上不同模型检测性能对比

    Table  4.   Comparison of detection performance of different models on embedded devices

    模型 mAP/% 帧率/(帧·s−1)
    YOLOv3-tiny 85.4 76
    YOLOv5 86.7 75
    FDG-YOLO 89.6 61
    下载: 导出CSV
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出版历程
  • 收稿日期:  2024-01-15
  • 录用日期:  2024-05-09
  • 网络出版日期:  2024-05-24
  • 整期出版日期:  2026-04-30

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