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可积物理GAN驱动的直升机尾传动轴承故障诊断

陈平,闫瑾,范腾飞,龙潜,尹爱军   

  1. 重庆大学
  • 收稿日期:2026-02-06 修回日期:2026-04-30 出版日期:2026-05-08 发布日期:2026-05-08
  • 通讯作者: 闫瑾
  • 基金资助:
    国家自然科学基金

Fault diagnosis of helicopter tail drive bearings using an integrable physical GAN

  • Received:2026-02-06 Revised:2026-04-30 Online:2026-05-08 Published:2026-05-08
  • Contact: Jin YAN
  • Supported by:
    National Natural Science Foundation of China

摘要: 针对直升机尾传动系统轴承故障诊断中故障样本稀缺导致的数据集不平衡问题,提出了可积的物理信息生成对抗网络(IE-PIGAN)模型。该模型在保留生成对抗网络(GAN)原有对抗损失与网络结构的基础上,通过将尾传动故障轴承的物理先验知识以积分方程形式嵌入生成器损失,并结合物理信息神经网络的数据损失对生成过程进行物理约束,实现了以随机噪声为输入、符合轴承物理特性的故障样本。实验结果表明,IE-PIGAN生成的信号在时域和频域与真实信号十分相似,其百分比均方根误差、均方根误差以及最大均值差异频域相关系数均比GAN低。将生成的数据加入到训练集中,卷积神经网络诊断准确率达91.7%,较无生成样本时提升8.4%,准确率优于去噪自编码器、变分自编码器等5种主流模型。生成数据量对增强效果呈先升后降趋势,与其他生成模型相比,IE-PIGAN在样本量超拐点后准确率下降速率最慢,有效缓解了直升机尾传动轴承故障样本的不平衡问题,提升了尾传动轴承故障诊断的精准性与鲁棒性。

关键词: 直升机, 尾传动, 滚动轴承, 样本不平衡, 故障诊断, 数据增强

Abstract: To address the problem of dataset imbalance caused by the scarcity of fault samples in the fault diagnosis of bearings in helicopter tail drive systems, we propose the Integrable Physical Information Generative Adversarial Network (IE-PIGAN) model. On the basis of retaining the original adversarial loss and network structure of Generative Adversarial Network (GAN), this model embeds the physical prior knowledge of tail drive fault bearings into the generator loss in the form of integral equations, and combines the data loss of physics-informed neural networks to impose physical constraints on the generation process, thus generating fault samples that take random noise as input and conform to the physical characteristics of bearings. Experimental results show that the signals generated by IE-PIGAN are highly similar to real signals in both time domain and frequency domain, and its percent root mean square error, root mean square error, and frequency-domain correlation coefficient of maximum mean discrepancy are all lower than those of GAN. When the generated data are added to the training set, the diagnostic accuracy of the convolutional neural network reaches 91.7%, which is 8.4% higher than that without generated samples, and the accuracy outperforms five mainstream models such as denoising autoencoders and variational autoencoders. The volume of generated data exhibits a trend of first increasing and then decreasing with respect to the enhancement effect. Compared with other generative models, IE-PIGAN has the slowest accuracy decline rate after the sample volume exceeds the inflection point. This model effectively alleviates the imbalance problem of fault samples for helicopter tail drive bearings, and improves the accuracy and robustness of tail drive bearing fault diagnosis.

Key words: helicopter, tail drive, rolling bearing, sample imbalance, fault diagnosis, data augmentation

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