Data Driven Comprehensive Performance Evaluation of Aeroengines: A Network Dynamic Approach

被引:0
|
作者
Wang, Yuting [1 ,2 ]
Liu, Feng [3 ]
Xi, Feng [3 ]
Wei, Bofei [3 ]
Duan, Dongli [4 ]
Cai, Zhiqiang [1 ,2 ]
Si, Shubin [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China
[2] Minist Ind & Informat Technol Peoples Republ China, Key Lab Ind Engn & Intelligent Mfg, Xian 710072, Peoples R China
[3] AECC Aviat Power Co Ltd, Xian 710005, Peoples R China
[4] Xian Univ Architecture & Technol, Sch Informat & Control Engn, Xian 710311, Peoples R China
来源
ENGINEERING | 2025年 / 46卷
基金
中国国家自然科学基金;
关键词
Comprehensive performance evaluation; Aeroengine performance; Network; Resilience; DATA ENVELOPMENT ANALYSIS; GAS-TURBINE DIAGNOSTICS; ARTIFICIAL-INTELLIGENCE; FUZZY-AHP; ENGINE; TOPSIS; METHODOLOGY; RESILIENCE; EFFICIENCY;
D O I
10.1016/j.eng.2024.11.024
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Aeroengines, often regarded as the heart of aircraft, are crucial for flight safety and performance. Comprehensive performance evaluation of aeroengines supports Prognostics and Health Management (PHM) and aeroengine digital engineering. Due to their highly integrated nature, aeroengines present challenges in performance evaluation because their test-run data are high-dimensional, large-scale, and exhibit strong nonlinear correlations among test indicators. To solve this problem, this study proposes a unified framework of the comprehensive performance evaluation of aeroengines to assess performance objectively and globally. Specifically, the network model and the dynamics model of aeroengine performance are constructed driven by test-run data, which can explain the patterns of system state changes and the internal relationship, and depict the system accurately. Based on that, three perturbations in the model are used to simulate three fault modes of aeroengines. Moreover, the comprehensive performance evaluation indexes of aeroengines are proposed to evaluate the performance dynamically from two dimensions, the coupling performance and the activity performance. Thirteen test-run qualified and four test-run failed aeroengines are used to validate and establish the qualified ranges. The results demonstrate that the comprehensive evaluation indexes can distinguish test-run qualified and test-run failed aeroengines. By changing the dynamic parameters, the comprehensive performance under any thrust and inlet guide vanes (IGV) angle can be estimated, broadening the test-run scenarios beyond a few typical states. This novel approach offers significant advancements for the comprehensive performance evaluation and management of aeroengines, paving the way for future PHM and aeroengine digital engineering developments. (c) 2024 THE AUTHORS. Published by Elsevier LTD on behalf of Chinese Academy of Engineering and Higher Education Press Limited Company. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:292 / 305
页数:14
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