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一种民航发动机滚动轴承故障预警方法
刘勇1,王朝2,周平3
1.中国民航大学 航空工程学院,天津 300300;2.中国商飞北京民用飞机技术研究中心,北京 102211;3.成都航利(集团)实业有限公司,四川 成都 640041
摘要:
为了提前感知滚动轴承故障,避免民用航空发动机非计划维护带来的损失,提出了一种故障预警方法。对轴承振动信号进行特征工程,提取其时域和频域特征,引入梯度提升决策树(Gradient boosting decision tree,GBDT)算法,量化了特征重要度;在特征相关性分析的基础上,利用核主成分分析(Kernel principal component analysis,KPCA)方法实现特征融合与主元提取,再次结合GBDT构建了故障预警模型,使用交叉验证法实现了模型泛化能力评估。结果表明:KPCA+GBDT模型的泛化性能显著,模型的F1分数高达0.991,对应的受试者工作特性(Receiver operating characteristic,ROC)曲线下面积的值为0.998,体现出该方法用于支撑航空发动机健康管理与维护决策工作的工程应用价值。
关键词:  航空发动机  滚动轴承  故障预警  核主成分分析  梯度提升决策树
DOI:10.13675/j.cnki.tjjs.200284
分类号:V232
基金项目:中国民航大学科研启动基金项目(2020KYQD76)。
An Early Warning Method for Rolling Bearing Fault of Civil Aero-Engine
LIU Yong1, WANG Chao2, ZHOU Ping3
1.College of Aeronautical Engineering,Civil Aviation University of China,Tianjin 300300,China;2.Beijing Aeronautical Science and Technology Research Institute of COMAC,Beijing 102211,China;3.Chengdu Holy Industry & Commerce Corp. Ltd (Group),Chengdu 640041,China
Abstract:
In order to detect the rolling bearing fault in advance and avoid the loss caused by unscheduled maintenance of civil aero-engine, a fault early warning method is proposed in the present work. Feature engineering is applied to bearing vibration signals, and its time and frequency domain features are extracted. The gradient boosting decision tree (GBDT) algorithm is adopted to quantify the feature importance. On the basis of feature correlation analysis, the kernel principal component analysis (KPCA) method is used to achieve feature fusion and principal component extraction. Combining with GBDT algorithm again, the fault early warning model is established. The cross-validation method is used to evaluate the generalization ability of the proposed model. The results show that the generalization performance of the KPCA+GBDT model is significant. The F1 score of the model is as high as 0.991, and the area under the receiver operating characteristic(ROC) curve, area under curve is 0.998, which means this model can be used to support the health management and maintenance decision-making work of civil aero-engine.
Key words:  Aero-engine  Rolling bearing  Fault early warning  Kernel principal component analysis  Gradient boosting decision tree