56 / 2015-12-31 21:30:18
Simulation of Engine’s Rub – impact Fault Detection Model Based on Flight Data
全文录用
Xiaohan WANG / Air Force Engineering University
During the status of real - time flight monitoring, it is related to the safety of flight that the accuracy of engine’s rub-impact fault detection under the strong vibration environments. Under the strong vibration environment, when engine goes to stationary state, the engine’s rub-impact fault is easy to happen, and they are often happened simultaneously. However, there is no correlation between the vibration signal faults. Traditional fault mining methods in the engine’s rub-impact fault detection process, it only can detect this fault the vibration signal, so that fault detection is not accurate.In order to solve this problem, the paper proposed an engine’s rub-impact fault detection method based on improved association rule mining. The associated clustering process are made with the data of engine’s rub-impact fault, to obtain the classification matrix of sample space and update the data of engine’s rub-impact fault. According to updated results, the association probability values of the data of engine’s rub - impact fault were calculated to obtain probabilistic decision. The association rules mining was made with data of aircraft’s rub-impact fault, so as to realize the optimized detection for the data of engine’s rub-impact fault. The experiment results show that using the improved association rules algorithm to detect the engine’s rotor-to station rub-impact fault under strong vibration environment, can greatly shorten the detection time,reduce the missing rate,and improve the detection accuracy.
重要日期
  • 会议日期

    05月21日

    2016

    05月22日

    2016

  • 12月31日 2015

    初稿截稿日期

  • 12月31日 2015

    提前注册日期

  • 01月10日 2016

    初稿录用通知日期

  • 01月20日 2016

    终稿截稿日期

  • 05月22日 2016

    注册截止日期

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