ZHOU Liang 1 , WANG Hua-wei 1 , XU Shan-shan 2 , WANG Qing-wei 1 , WANG Ying 1.Aeroengine Fault Diagnosis Based on Cluster Analysis of Lubricant Wear Particles[J].航空发动机,2024,50(6):113-119
Aeroengine Fault Diagnosis Based on Cluster Analysis of Lubricant Wear Particles
DOI:
Key Words:identification clustering  fault diagnosis  condition monitoring  particle swarm optimization  support vector machine  aeroengine
Author NameAffiliation
ZHOU Liang 1 , WANG Hua-wei 1 , XU Shan-shan 2 , WANG Qing-wei 1 , WANG Ying 1 1. School of Civil Aviation Nanjing University of Aeronautics and Astronautics Nanjing 211100 China 2. School of Public Administration Shandong Normal University Jinan 250300 China 
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Abstract:In order to effectively analyze the lubricating oil status and realize the wear status monitoring of key components of aeroengine based on lubricating oil status analysis, aeroengine fault diagnosis research based on lubricating oil abrasive particle clustering analysis was carried out. The principal component analysis algorithm is used to extract the key feature parameters of lubricating oil abrasive particles. Combined with the key feature parameters, the support vector machine model is used to perform cluster identification of lubricat? ing oil abrasive particles. By analyzing the improved particle swarm algorithm, the support vector machine model is optimized using the adaptive weight particle swarm algorithm and the asynchronous shrinkage factor particle swarm algorithm to improve the accuracy of clustering. Taking lubricating oil spectral data as an example, a lubricating oil abrasive particle clustering test was conducted. The test results show that through two improved particle swarm optimization support vector machine model simulations, the cluster identification of abrasive particles in aeroengine lubricating oil can be achieved, with an identification accuracy as high as 99.7%, and the monitoring and diagnosis results are consistent with actual faults. The results provide a basis for oil condition monitoring and fault diagnosis of aeroengine.
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