Vibration Characteristics of a Dual-Rotor System with Non-Concentricity

A finite element model of an aero-engine dual-rotor system with intermediate bearing supported by six bearings is set up. Three modes of non-concentricity caused by the assembly process are defined, namely parallel non-concentricity, front deflection angle non-concentricity and rear deflection angle...

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Autores principales: Shengliang Hou, Lei Hou, Shiwei Dun, Yufeng Cai, Yang Yang, Yushu Chen
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Lenguaje:EN
Publicado: MDPI AG 2021
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Acceso en línea:https://doaj.org/article/f08ec11b5e7c40d9b1f5b7337c47c41a
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spelling oai:doaj.org-article:f08ec11b5e7c40d9b1f5b7337c47c41a2021-11-25T18:12:01ZVibration Characteristics of a Dual-Rotor System with Non-Concentricity10.3390/machines91102512075-1702https://doaj.org/article/f08ec11b5e7c40d9b1f5b7337c47c41a2021-10-01T00:00:00Zhttps://www.mdpi.com/2075-1702/9/11/251https://doaj.org/toc/2075-1702A finite element model of an aero-engine dual-rotor system with intermediate bearing supported by six bearings is set up. Three modes of non-concentricity caused by the assembly process are defined, namely parallel non-concentricity, front deflection angle non-concentricity and rear deflection angle non-concentricity. The influence of the non-concentricity on the vibration characteristics of the dual-rotor system is investigated in detail. The results show that the parallel non-concentricity and the front deflection angle non-concentricity have a significant influence on the bending vibration modals of the high-pressure rotor and the low-pressure rotor, but have little influence on the local vibration modals of the rotors. With the increase in the magnitude of the non-concentricity, the natural frequencies of the bending modals decrease continuously, and the mode shapes of bending modals and that of local modals may be interchanged, leading to the emergence of bending modals in advance. Therefore, the key parameters to be controlled in the assembly process are the parallel non-concentricity and the front deflection angle non-concentricity. In order to prevent the bending modal of the dual-rotor system from appearing in advance, it is necessary to control the parallel non-concentricity within 2 mm and the front deflection angle non-concentricity amount within 0.18°.Shengliang HouLei HouShiwei DunYufeng CaiYang YangYushu ChenMDPI AGarticledual-rotor systemnon-concentricity in the assembly processfinite element modelvibration characteristicsMechanical engineering and machineryTJ1-1570ENMachines, Vol 9, Iss 251, p 251 (2021)
institution DOAJ
collection DOAJ
language EN
topic dual-rotor system
non-concentricity in the assembly process
finite element model
vibration characteristics
Mechanical engineering and machinery
TJ1-1570
spellingShingle dual-rotor system
non-concentricity in the assembly process
finite element model
vibration characteristics
Mechanical engineering and machinery
TJ1-1570
Shengliang Hou
Lei Hou
Shiwei Dun
Yufeng Cai
Yang Yang
Yushu Chen
Vibration Characteristics of a Dual-Rotor System with Non-Concentricity
description A finite element model of an aero-engine dual-rotor system with intermediate bearing supported by six bearings is set up. Three modes of non-concentricity caused by the assembly process are defined, namely parallel non-concentricity, front deflection angle non-concentricity and rear deflection angle non-concentricity. The influence of the non-concentricity on the vibration characteristics of the dual-rotor system is investigated in detail. The results show that the parallel non-concentricity and the front deflection angle non-concentricity have a significant influence on the bending vibration modals of the high-pressure rotor and the low-pressure rotor, but have little influence on the local vibration modals of the rotors. With the increase in the magnitude of the non-concentricity, the natural frequencies of the bending modals decrease continuously, and the mode shapes of bending modals and that of local modals may be interchanged, leading to the emergence of bending modals in advance. Therefore, the key parameters to be controlled in the assembly process are the parallel non-concentricity and the front deflection angle non-concentricity. In order to prevent the bending modal of the dual-rotor system from appearing in advance, it is necessary to control the parallel non-concentricity within 2 mm and the front deflection angle non-concentricity amount within 0.18°.
format article
author Shengliang Hou
Lei Hou
Shiwei Dun
Yufeng Cai
Yang Yang
Yushu Chen
author_facet Shengliang Hou
Lei Hou
Shiwei Dun
Yufeng Cai
Yang Yang
Yushu Chen
author_sort Shengliang Hou
title Vibration Characteristics of a Dual-Rotor System with Non-Concentricity
title_short Vibration Characteristics of a Dual-Rotor System with Non-Concentricity
title_full Vibration Characteristics of a Dual-Rotor System with Non-Concentricity
title_fullStr Vibration Characteristics of a Dual-Rotor System with Non-Concentricity
title_full_unstemmed Vibration Characteristics of a Dual-Rotor System with Non-Concentricity
title_sort vibration characteristics of a dual-rotor system with non-concentricity
publisher MDPI AG
publishDate 2021
url https://doaj.org/article/f08ec11b5e7c40d9b1f5b7337c47c41a
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AT leihou vibrationcharacteristicsofadualrotorsystemwithnonconcentricity
AT shiweidun vibrationcharacteristicsofadualrotorsystemwithnonconcentricity
AT yufengcai vibrationcharacteristicsofadualrotorsystemwithnonconcentricity
AT yangyang vibrationcharacteristicsofadualrotorsystemwithnonconcentricity
AT yushuchen vibrationcharacteristicsofadualrotorsystemwithnonconcentricity
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