Aero Engine Gas Path Fault Prediction Based on Multi-sensor Information Fusion

被引:0
|
作者
Yang Xiaohong [1 ]
Guo Haifeng [1 ]
Zhang Jing [2 ]
Xu Jing [3 ]
Zhao Dandan [1 ]
机构
[1] Air Force Aviat Univ, Dep Aircraft Controller, Changchun 130022, Peoples R China
[2] Air Force Aviat Univ, Int Students Training Dept, Changchun 130022, Peoples R China
[3] Jilin Univ, Hosp 1, Dept Neurol Internal Med, Changchun 130012, Peoples R China
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
For the problem of aero engine gas path fault diagnosis, the diagnosis results of RBF neural network, BP neural network and support vector machine (SVM) are fused at decision level with the D-S evidence theory, the results show that D-S evidence theory can achieve better diagnosis efticiency than the other three theories in separation, and it can reduce the misdiagnosis rate and improve the diagnostic performance. The fault prediction method based on information fusion can avoid the disadvantage of a single method. This method provides a determination to improve the reliability of aero engine, and the best maintenance decision reference and prolongs service life.
引用
收藏
页码:49 / 52
页数:4
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