中国航空学报(英文版)2024,Vol.37Issue(5) :533-557.DOI:10.1016/j.cja.2023.09.011

Knowledge and data jointly driven aeroengine gas path performance assessment method

Zhe WANG Xuyun FU Rui ZHANG Zhengfeng BAI Xiangzhao XIA Wei JIANG
中国航空学报(英文版)2024,Vol.37Issue(5) :533-557.DOI:10.1016/j.cja.2023.09.011

Knowledge and data jointly driven aeroengine gas path performance assessment method

Zhe WANG 1Xuyun FU 1Rui ZHANG 2Zhengfeng BAI 3Xiangzhao XIA 1Wei JIANG1
扫码查看

作者信息

  • 1. Department of Mechanical Engineering,Harbin Institute of Technology,Weihai 264209,China;Weihai Key Laboratory of Intelligent Operation and Maintenance,Harbin Institute of Technology,Weihai 264209,China
  • 2. Control System Design Laboratory,AECC ShenYang Engine Research Institute,Shenyang 110015,China
  • 3. Department of Mechanical Engineering,Harbin Institute of Technology,Weihai 264209,China
  • 折叠

Abstract

Aeroengines,as the sole power source for aircraft,play a vital role in ensuring flight safety.The gas path,which represents the fundamental pathway for airflow within an aeroengine,directly impacts the aeroengine's performance,fuel efficiency,and safety.Therefore,timely and accurate evaluation of gas path performance is of paramount importance.This paper proposes a knowledge and data jointly driven aeroengine gas path performance assessment method,combining Fingerprint and gas path parameter deviation values.Firstly,Fingerprint is used to correct gas path parameter deviation values,eliminating parameter shifts caused by non-component performance degradation.Secondly,coarse errors are removed using the Romanovsky criterion for short-term data divided by an equal-length overlapping sliding window.Thirdly,an Ensemble Empirical Mode Decomposition and Non-Local Means(EEMD-NLM)filtering method is designed to"clean"data noise,completing the preprocessing for gas path parameter deviation values.Afterward,based on the characteristics of gas path parameter deviation values,a Dynamic Temporary Blended Network(DTBN)model is built to extract its temporal features,cascaded with Multi-Layer Perceptron(MLP),and combined with Fingerprint to construct a Dynamic Temporary Blended AutoEncoder(DTB-AutoEncoder).Eventually,by training this improved autoencoder,the aeroengine gas path multi-component performance assessment model is formed,which can sufficiently decouple the nonlinear mapping relationship between aeroengine gas path multi-component performance degra-dation and gas path parameter deviation values,thereby achieving the performance assessment of engine gas path components.Through practical application cases,the effectiveness of this model in assessing the aeroengine gas path multi-component performance is verified.

Key words

Performance assessment/Aeroengine/Fingerprint/Gas path parameter devia-tion values/Jointly drive

引用本文复制引用

基金项目

National Key Research and Development Program of China(2020YFB1709800)

National Science and Technology Major Project(J2019-Ⅰ-0001-0001)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
段落导航相关论文