Fault diagnosis of aeroengine bearings using multi-source fusion STFT-IncepNext method
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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。
Abstract:To address the challenge of reliably monitoring aviation engine bearing faults under complex operating conditions with limited information from a single sensor, the STFT-IncepNext model was proposed for bearing fault diagnosis. Initially, sensor data from different positions within the same time window were concatenated to enrich the vibration information of bearings across various spatial dimensions. Subsequently, to capture the transient changes of fault components in the vibration signal, the short-time Fourier transform (STFT) was applied to convert multi-sensor vibration signals into time-frequency representations. Finally, a lightweight IncepNext network extracted global features of fault information embedded in the time-frequency representations, and a Softmax classifier identified the fault category. Experimental results demonstrated that the proposed approach effectively enhanced signal fault characteristics, and improved the discriminability of vibration features under various bearing states. Under specific experimental conditions, the method achieved an accuracy rate of 100% for diagnosing vibration faults in aeroengine bearings. Compared with STFT-EdgeNeXt, STFT-ResNeXt, STFT-ShuffleNet, and STFT-ResNet18, the method exhibited superior performance, providing a feasible approach for diagnosing faults in aeroengine bearings.
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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1 NI_2(轴向) 平行齿轮箱中间
轴轴承端盖加速度2 NI_3(水平径向) 加速度3 NI_4(垂直径向) 加速度4 NI_5 平行齿轮箱右侧箱体
(靠上轴承)加速度5 NI_6 承重台面(靠平行齿轮箱) 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 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 4 800 1 滚动体 4 800 2 联合 4 800 3 内圈 4 800 4 外圈 4 800 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 -
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