Volume 36 Issue 1
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Article Navigation >  Journal of Aerospace Power  > 2021  >  36(1): 167-175
HAN Jinchang, ZUO Yanfei, FENG Kun. Response mechanism of thin-walled casing support system under periodic rubbing exciation[J]. Journal of Aerospace Power, 2021, 36(1): 167-175. doi: 10.13224/j.cnki.jasp.2021.01.019
Citation: HAN Jinchang, ZUO Yanfei, FENG Kun. Response mechanism of thin-walled casing support system under periodic rubbing exciation[J]. Journal of Aerospace Power, 2021, 36(1): 167-175. doi: 10.13224/j.cnki.jasp.2021.01.019
shu

Response mechanism of thin-walled casing support system under periodic rubbing exciation

doi: 10.13224/j.cnki.jasp.2021.01.019
  • 1.

    Beijing Key Laboratory of High-end Mechanical Equipment Health Monitoring and ,Self-Recovery,Beijing University of Chemical Technology,Beijing 100029,China

  • 2.

    Key Laboratory of Engine Health Monitoring-control and Networking of Ministry of Education,Beijing University of Chemical Technology,Beijing 100029,China

  • Received Date: 2020-06-17
  • Publish Date: 2021-01-28
    Abstract
  • In view of the complex dynamic response law of the engine’s thin-walled casing support system under rubbing excitation and the difficulty of character identification of rubbing fault based on the vibration signal of the casing, a numerical simulation method for the mechanism analysis of the fault characteristics was presented. An equivalent dynamic three-dimensional solid model of the thin-walled casing system was established and the rubbing excitation was simplified by equivalent mechanics. Then the periodic rubbing fault was simulated numerically with transient dynamics method. Based on analysis of the inherent characteristics of the system, the time domain and frequency domain response characteristics were studied and the rubbing fault feature was obtained. The dominant frequency of the casing displacement vibration signal was the low-order natural frequency of the system, and the dominant frequency of the acceleration vibration signal was the rub-impact excitation frequency and its multiples. The above conclusions can be used as the basis for rub-impact faults and provide references for early fault diagnosis.

     

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