Volume 32 Issue 9
Sep.  2017
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Fault sensitivity analysis and fusion technology for vibration features of aero-engine rolling bearings[J]. Journal of Aerospace Power, 2017, 32(9): 2205-2218. doi: 10.13224/j.cnki.jasp.2017.09.020
Citation: Fault sensitivity analysis and fusion technology for vibration features of aero-engine rolling bearings[J]. Journal of Aerospace Power, 2017, 32(9): 2205-2218. doi: 10.13224/j.cnki.jasp.2017.09.020

Fault sensitivity analysis and fusion technology for vibration features of aero-engine rolling bearings

doi: 10.13224/j.cnki.jasp.2017.09.020
  • Received Date: 2016-01-13
  • Publish Date: 2017-09-28
  • A method of multifeatures fusion based on normalized Euclidean distance was proposed to meet the requirement of monitoring aeroengine rolling bearing real time condition. Firstly, the bearing fault simulation experiments were carried out while the fault sensitivity of the features before and after fusion was analysed by introducing a quantitative evaluation index of fault sensitivity. Then, the proposed method was compared with the principal component analysis, support vector data description and support vector distribution estimation. Finally, the bearing fatigue accelerated experiment was carried out, and the proposed fusion method was applied to the aeroengine rolling bearing condition monitoring. Experimental results show that compared with principal component analysis, support vector data description and support vector distribution estimation, the fault sensitivity of fusion value based on normalized Euclidean distance is higher. For different types and different stages of the bearing fault, the fusion value obtained by proposed method is more sensitive, which is more suitable to be an index of the bearing condition monitoring, compared with the effective value.

     

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