Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework

In order to improve the accuracy and calculation efficiency of aeroengine rotor vibration reliability analysis, a time-varying rotor vibration reliability analysis method under the aeroengine operating state is proposed. Aiming at the highly nonlinear and strong coupling of factors affecting the rel...

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Main Authors: Jia-Qi Liu, Yun-Wen Feng, Cheng Lu, Wei-Huang Pan, Da Teng
Format: Article
Language:English
Published: Wiley 2021-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2021/9910601
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author Jia-Qi Liu
Yun-Wen Feng
Cheng Lu
Wei-Huang Pan
Da Teng
author_facet Jia-Qi Liu
Yun-Wen Feng
Cheng Lu
Wei-Huang Pan
Da Teng
author_sort Jia-Qi Liu
collection DOAJ
description In order to improve the accuracy and calculation efficiency of aeroengine rotor vibration reliability analysis, a time-varying rotor vibration reliability analysis method under the aeroengine operating state is proposed. Aiming at the highly nonlinear and strong coupling of factors affecting the reliability of aeroengine rotor vibration, an intelligent neural network modeling framework (short form-INNMF) is proposed. The proposed method is based on DEA, with QAR information as the analysis data, and four factors including engine working state, fuel/oil working state, aircraft flight state, and external conditions are considered to analyse the rotor vibration reliability. INNMF is based on the artificial neural network (ANN) algorithm through improved particle swarm optimization (PSO) algorithm and Bayesian Regularization (BR) optimization. Through the analysis of the rotor vibration reliability of the B737-800 aircraft during a flight mission from Beijing to Urumqi, the time-varying rotor vibration reliability was obtained, which verified the effectiveness and feasibility of the method. The comparison of INNMF, random forest (RF), and ANN shows that INNMF improves analysis accuracy and calculation efficiency. The proposed method and framework can provide useful references for aeroengine rotor vibration analysis, special treatment, maintenance, and design.
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institution Kabale University
issn 1070-9622
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language English
publishDate 2021-01-01
publisher Wiley
record_format Article
series Shock and Vibration
spelling doaj-art-87e1b93b715e4d909a3c2b039916051a2025-02-03T06:07:38ZengWileyShock and Vibration1070-96221875-92032021-01-01202110.1155/2021/99106019910601Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling FrameworkJia-Qi Liu0Yun-Wen Feng1Cheng Lu2Wei-Huang Pan3Da Teng4School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaIn order to improve the accuracy and calculation efficiency of aeroengine rotor vibration reliability analysis, a time-varying rotor vibration reliability analysis method under the aeroengine operating state is proposed. Aiming at the highly nonlinear and strong coupling of factors affecting the reliability of aeroengine rotor vibration, an intelligent neural network modeling framework (short form-INNMF) is proposed. The proposed method is based on DEA, with QAR information as the analysis data, and four factors including engine working state, fuel/oil working state, aircraft flight state, and external conditions are considered to analyse the rotor vibration reliability. INNMF is based on the artificial neural network (ANN) algorithm through improved particle swarm optimization (PSO) algorithm and Bayesian Regularization (BR) optimization. Through the analysis of the rotor vibration reliability of the B737-800 aircraft during a flight mission from Beijing to Urumqi, the time-varying rotor vibration reliability was obtained, which verified the effectiveness and feasibility of the method. The comparison of INNMF, random forest (RF), and ANN shows that INNMF improves analysis accuracy and calculation efficiency. The proposed method and framework can provide useful references for aeroengine rotor vibration analysis, special treatment, maintenance, and design.http://dx.doi.org/10.1155/2021/9910601
spellingShingle Jia-Qi Liu
Yun-Wen Feng
Cheng Lu
Wei-Huang Pan
Da Teng
Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
Shock and Vibration
title Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
title_full Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
title_fullStr Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
title_full_unstemmed Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
title_short Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
title_sort vibration reliability analysis of aeroengine rotor based on intelligent neural network modeling framework
url http://dx.doi.org/10.1155/2021/9910601
work_keys_str_mv AT jiaqiliu vibrationreliabilityanalysisofaeroenginerotorbasedonintelligentneuralnetworkmodelingframework
AT yunwenfeng vibrationreliabilityanalysisofaeroenginerotorbasedonintelligentneuralnetworkmodelingframework
AT chenglu vibrationreliabilityanalysisofaeroenginerotorbasedonintelligentneuralnetworkmodelingframework
AT weihuangpan vibrationreliabilityanalysisofaeroenginerotorbasedonintelligentneuralnetworkmodelingframework
AT dateng vibrationreliabilityanalysisofaeroenginerotorbasedonintelligentneuralnetworkmodelingframework