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논문 기본 정보

자료유형
학술저널
저자정보
(한국항공대학교) (한국항공대학교) (한국항공대학교) (LIG넥스원) (LIG넥스원) (국방과학연구소) (한국항공대학교)
저널정보
한국신뢰성학회 신뢰성응용연구 신뢰성응용연구 제21권 제4호
발행연도
수록면
329 - 340 (12page)
DOI
10.33162/JAR.2021.12.21.4.329

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초록· 키워드

Purpose: Gear teeth in the rotary geared actuator of the unmanned aerial vehicle, experience crack propagation because of its harsh operating conditions. To prevent the failure of catastrophic events, this study proposes a diagnostic approach for various gear crack levels based on the built-in and add-on sensor signal.
Methods: A downsized planetary gearbox test rig was prepared, in which the motor position, current, and vibration signals were acquired for the normal and 4 different crack-induced states. Signals were filtered around the region of resonance frequencies by spectral kurtosis and the features for the health state were extracted. Then, feature selection was conducted based on the correlation with fault levels. Finally, the Artificial Neural Network (ANN) model was constructed to identify different fault sizes of the cracks, and K-fold validation was adopted to optimize the parameters of the ANN model.
Results: Among the various signals, the vibration from the add-on sensor and a position from the built-in sensor exhibited high performance compared to the current signal. The features after band-pass filtering yielded a high correlation with fault severity.
Conclusion: The proposed method successfully diagnosed different fault severities of gear cracks in the planetary gearbox by using both the built-in and add-on signals.
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목차

  1. 1. 서론
  2. 2. 본론
  3. 3. 유성감속기 고장진단
  4. 4. 결론
  5. References

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