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Publishing Language: Chinese

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

Shuyu CAI( )Chong HE
College of Aeronautical Engineering,Civil Aviation University of China,Tianjin 300300,China
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Abstract

In response to the issues of poor real-time performance and low detection accuracy when deploying deep learning models for aero-engine damage detection on embedded devices, this paper introduces the FDG-YOLO lightweight model for aviation engine damage detection. Firstly, FasterNet was introduced to restructure the backbone network of YOLOv5, addressing the issue of large parameter count in the backbone network. Second, depth-wise separable convolutions were used to eliminate superfluous parameters in the neck network of YOLOv5 by improving ordinary convolutions. In order to improve the model's expressive power and receptive field, the original C3 structure was replaced with the GS C3 structure, which was built concurrently based on GSConv. Finally, experiments were conducted and validated on an aviation engine damage dataset. In the end, experiments were conducted and validated on an aero-engine damage dataset. The findings show that the FDG-YOLO model reduces the number of parameters by 52.5% and the giga floating-point operations per second by 66% when compared to the original model. On embedded devices, the mean average precision (mAP) reaches 89.6%, surpassing other lightweight models. The frames per second achieves 61, making the detection speed suitable for the engine damage image acquisition rate. It more effectively satisfies aero-engine damage detection's intelligent application criteria.

CLC number: V263.6;TP391.41 Document code: A Article ID: 1001-5965(2026)04-1055-09

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Journal of Beijing University of Aeronautics and Astronautics
Pages 1055-1063

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Cite this article:
CAI S, HE C. Damage detection method for aero-engine based on FDG-YOLO lightweight model. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(4): 1055-1063. https://doi.org/10.13700/j.bh.1001-5965.2024.0024

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Received: 15 January 2024
Published: 24 May 2024
© Journal of Beijing University of Aeronautics and Astronautics