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INTELLIGENT FUSION FOR AEROENGINE WEAR FAULT DIAGNOSIS 被引量:3
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作者 陈果 杨虞微 左洪福 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2006年第4期297-303,共7页
Four common oil analysis techniques, including the ferrography analysis (FA), the spectrometric oil analysis (SOA), the particle count analysis (PCA), and the oil quality testing (OQT), are used to implement t... Four common oil analysis techniques, including the ferrography analysis (FA), the spectrometric oil analysis (SOA), the particle count analysis (PCA), and the oil quality testing (OQT), are used to implement the military aeroengine wear fault diagnosis during the test drive process. To improve the precision and the reliability of the diagnosis, the aeroengine wear fault fusion diagnosis method based on the neural networks (NN) and the Dempster-Shafter (D-S) evidence theory is proposed. Firstly, according to the standard value of the wear limit, original data are pre-processed into Boolean values. Secondly, sub-NNs are established to perform the single diagnosis, and their training samples are dependent on experiences from experts. After each sub-NN is trained, diagnosis results are obtained. Thirdly, the diagnosis results of each sub-NN are considered as the basic probability allocation value to faults. The improved D-S evidence theory is applied to the fusion diagnosis, and the final fusion results are obtained. Finally, the method is verified by a diagnosis example. 展开更多
关键词 wear fault diagnosis data fusion neural network D-S evidence theory aeroengine
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