Volume 45 Issue 6
Jun.  2019
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BAO Mengyao, DING Shuiting, LI Guoet al. Classification of key influence factors for failure of turbo supercharged piston aeroengine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1071-1080. doi: 10.13700/j.bh.1001-5965.2018.0597(in Chinese)
Citation: BAO Mengyao, DING Shuiting, LI Guoet al. Classification of key influence factors for failure of turbo supercharged piston aeroengine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1071-1080. doi: 10.13700/j.bh.1001-5965.2018.0597(in Chinese)

Classification of key influence factors for failure of turbo supercharged piston aeroengine

doi: 10.13700/j.bh.1001-5965.2018.0597
Funds:

Joint Fund of National Natural Science Foundation of China and the Civil Aviation Administration of China U1833109

More Information
  • Corresponding author: BAO Mengyao, E-mail: baomengyao@camic.cn
  • Received Date: 17 Oct 2018
  • Accepted Date: 04 Jan 2019
  • Publish Date: 20 Jun 2019
  • Using turbocharging technology dramatically increases the complexity of piston engine systems and the safety issues associated with turbocharger are becoming urgent. A typical two-stage turbo supercharged piston engine is considered and the judgment method for failure of incentives is focused in this study. Based on the built whole engine system model, a modified correspondence analysis method is proposed, which implements the classification of factors on the failure modes. The results show that the key influence factors and potential causes of coupling failure for turbo supercharged piston engine in actual motion can be judged through changed column contour coordinates in proposed classification method. The test presents that the diameter of exhaust valve is the dominant factors for safety margin boundary and needs to be controlled primarily.

     

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