中介轴承寿命预测方法与寿命试验研究
[Abstract]:As the key parts of aero-engine, intermediate bearings work in the harsh environment of high temperature, high speed, heavy load and strong vibration. The reliability of their performance directly restricts flight safety and aircraft performance. Therefore, the running law of intermediary bearing is deeply studied, the real-time condition monitoring is carried out, the fault diagnosis and life prediction of intermediary bearing are realized, and the maintenance cost is reduced according to the situation. It is of great practical significance to improve the level of aero-engine health management. In this paper, the life prediction theory based on Cox proportional fault model is studied, and the life test bench is designed to carry out the life test, and the corresponding intermediate bearing condition monitoring and life prediction system is developed. The main contents of this paper are as follows: first, this paper discusses the background of the topic, the life prediction theory and the domestic and foreign research status of the bearing test bed, introduces the general situation of the intermediate bearing, analyzes the common failure forms of the intermediate bearing. The vibration mechanism of bearing and the extraction and analysis methods of vibration signals in time domain, frequency domain and time frequency domain are studied. Secondly, the reliability and service life are introduced, the life prediction method of proportional failure rate model based on Weibull distribution is studied, and the best life reference function is selected. Parameter estimation method based on maximum likelihood estimation model, covariable selection method based on correlation analysis and covariable trend prediction method based on AR model are studied. The proportional failure rate model based on Weibull distribution is established and the reliability function diagram is given. The reliability life is obtained and the validity and reliability of the model are verified. Then, taking the intermediate bearing as the main research object, simulates the actual supporting structure and working environment of the aeroengine, designs the double rotor test bench of the intermediate bearing, carries out the acceleration life test of the intermediate bearing, The suitable acceleration stress is analyzed and selected, the selection of stop threshold is studied deeply, the monitoring scheme of intermediate bearing accelerated life test is designed, and the selection and arrangement of sensor are described in detail. The typical life test was carried out, and the life test of intermediate bearing with different damage degree was made. Finally, an intermediate bearing condition monitoring and life prediction system is developed. This paper introduces the software and hardware development environment of the system, according to the requirements of the monitoring scheme, the state monitoring part realizes temperature monitoring, rotational speed monitoring, displacement monitoring and vibration monitoring, and the life prediction system realizes the feature extraction of vibration signal. Covariable selection and trend analysis of the model, parameter estimation and reliability life estimation of the model. The system also realizes user login, alarm setting, data saving and good man-machine relationship.
【学位授予单位】:大连理工大学
【学位级别】:硕士
【学位授予年份】:2016
【分类号】:V263.6
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