Volume 45 Issue 6
Jun.  2019
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TAN Zhixue, ZHONG Shisheng, LIN Linet al. Commercial aircraft engine post-repairing performance prediction based on fusion of multisource data[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1106-1113. doi: 10.13700/j.bh.1001-5965.2018.0557(in Chinese)
Citation: TAN Zhixue, ZHONG Shisheng, LIN Linet al. Commercial aircraft engine post-repairing performance prediction based on fusion of multisource data[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1106-1113. doi: 10.13700/j.bh.1001-5965.2018.0557(in Chinese)

Commercial aircraft engine post-repairing performance prediction based on fusion of multisource data

doi: 10.13700/j.bh.1001-5965.2018.0557
Funds:

National Natural Science Foundation of China U1533202

the Major Project of Civil Aviation Administration of China MHRD20150104

Shandong Independent Innovation and Achievements Transformation Fund 2014CGZH1101

More Information
  • Corresponding author: ZHONG Shisheng, E-mail: zhongss@hit.edu.cn
  • Received Date: 19 Sep 2018
  • Accepted Date: 04 Jan 2019
  • Publish Date: 20 Jun 2019
  • To solve the problem of multisource heterogeneous data fusion in commercial aircraft engine post-repairing exhaust gas temperature margin prediction, a combined method of convolutional auto-encoder and extreme gradient boost model was proposed. This method uses the proposed cross entropy increasing factor to regularize the parameter order in the multi-dimensional engine sensor parameter series observed before repairing, and then uses convolutional auto-encoder to extract features from the regularized parameter series and engine workscope data. With the combined feature composed of the extracted features and the features representing engine using time, extreme gradient boost model is trained in order to predict engine post-repairing performance and estimate the importance of influential factors. The experiment performed on the prediction of the post-repairing performance of an engine fleet proved that the proposed method achieves higher prediction precision than prediction methods supported by one-dimentional parameter series and can predict engine post-repairing exhaust gas temperature margin with an average relative error no higher than 8.3%.

     

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