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Open Access

A step parameters prediction model based on transfer process neural network for exhaust gas temperature estimation after washing aero-engines

Zhiqi YANaShisheng ZHONGa( )Lin LINaZhiquan CUIbMinghang ZHAOc
School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China
Department of Vehicle Engineering, Harbin Institute of Technology, Weihai 264209, China
School of Naval Architecture and Ocean Engineering, Harbin Institute of Technology, Weihai 264209, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The prediction of Exhaust Gas Temperature Margin (EGTM) after washing aero-engines can provide a theoretical basis for airlines not only to evaluate the energy-saving effect and emission reduction, but also to formulate reasonable maintenance plans. However, the EGTM encounters step changes after washing aeroengines, while, in the traditional models, a persistence tendency exists between the prediction results and the previous data, resulting in low accuracy in prediction. In order to solve the problem, this paper develops a step parameters prediction model based on Transfer Process Neural Networks (TPNN). Especially, “step parameters” represent the parameters that can reflect EGTM step changes. They are analyzed in this study, and thus the model concentrates on the prediction of step changes rather than the extension of data trends. Transfer learning is used to handle the problem that few cleaning records result in few step changes for model learning. In comparison with Long Short-Term Memory (LSTM) and Kernel Extreme Learning Machine (KELM) models, the effectiveness of the proposed method is verified on CFM56-5B engine data.

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Chinese Journal of Aeronautics
Pages 98-111

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Cite this article:
YAN Z, ZHONG S, LIN L, et al. A step parameters prediction model based on transfer process neural network for exhaust gas temperature estimation after washing aero-engines. Chinese Journal of Aeronautics, 2022, 35(3): 98-111. https://doi.org/10.1016/j.cja.2021.07.035

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Received: 20 October 2020
Revised: 11 November 2020
Accepted: 15 January 2021
Published: 21 October 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).