Vibration responses of a two-span three-support rotor system with sliding bearing elevation change

<p>The two-span three-support rotor is a typical structure in rotating machinery such as steam turbines and water pumps. The alteration in bearing elevation can result in oil film instability, rotor rub impact, and other malfunctions. In extreme cases, this can cause excessive wear of coupling...

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Main Authors: Z. Zhou, G. Bin, C. Li, Y. Gao, M. Bayjid Md
Format: Article
Language:English
Published: Copernicus Publications 2025-07-01
Series:Mechanical Sciences
Online Access:https://ms.copernicus.org/articles/16/375/2025/ms-16-375-2025.pdf
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author Z. Zhou
G. Bin
C. Li
Y. Gao
M. Bayjid Md
author_facet Z. Zhou
G. Bin
C. Li
Y. Gao
M. Bayjid Md
author_sort Z. Zhou
collection DOAJ
description <p>The two-span three-support rotor is a typical structure in rotating machinery such as steam turbines and water pumps. The alteration in bearing elevation can result in oil film instability, rotor rub impact, and other malfunctions. In extreme cases, this can cause excessive wear of couplings and other components, leading to accidents. This study derives the dynamic equation of a two-span three-support rotor that accounts for variations in bearing elevation. Meanwhile, the influence of different sliding bearing elevations on the misalignment excitation of the coupling and the stiffness damping coefficient of the bearing is considered, and the vibration response of each bearing is also investigated. Corresponding experiments are designed and conducted to validate the findings. The findings indicate that after raising the elevation of bearing 3 from 1.5 to 2 mm, the amplitude of the fundamental frequency (<span class="inline-formula">1×</span>) at bearing 2 is reduced by 438 %, whereas the amplitude at the second harmonic (<span class="inline-formula">2×</span>) is increased by 128 %. This increase in misalignment excitation causes the axis orbit of disk 1 to change from a crescent shape to a petal shape. This study offers theoretical insights and empirical data that may assist in the structural design and fault diagnosis of two-span three-support rotors.</p>
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institution Kabale University
issn 2191-9151
2191-916X
language English
publishDate 2025-07-01
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series Mechanical Sciences
spelling doaj-art-87f8179007cd41e094f5b6b035b578912025-08-20T03:28:18ZengCopernicus PublicationsMechanical Sciences2191-91512191-916X2025-07-011637539010.5194/ms-16-375-2025Vibration responses of a two-span three-support rotor system with sliding bearing elevation changeZ. Zhou0G. Bin1C. Li2Y. Gao3M. Bayjid Md4Hunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment, Hunan University of Science and Technology, Xiangtan 411201, ChinaHunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment, Hunan University of Science and Technology, Xiangtan 411201, ChinaHunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment, Hunan University of Science and Technology, Xiangtan 411201, ChinaHunan Electric Power Co Ltd, Xiangtan 411201, ChinaHunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment, Hunan University of Science and Technology, Xiangtan 411201, China<p>The two-span three-support rotor is a typical structure in rotating machinery such as steam turbines and water pumps. The alteration in bearing elevation can result in oil film instability, rotor rub impact, and other malfunctions. In extreme cases, this can cause excessive wear of couplings and other components, leading to accidents. This study derives the dynamic equation of a two-span three-support rotor that accounts for variations in bearing elevation. Meanwhile, the influence of different sliding bearing elevations on the misalignment excitation of the coupling and the stiffness damping coefficient of the bearing is considered, and the vibration response of each bearing is also investigated. Corresponding experiments are designed and conducted to validate the findings. The findings indicate that after raising the elevation of bearing 3 from 1.5 to 2 mm, the amplitude of the fundamental frequency (<span class="inline-formula">1×</span>) at bearing 2 is reduced by 438 %, whereas the amplitude at the second harmonic (<span class="inline-formula">2×</span>) is increased by 128 %. This increase in misalignment excitation causes the axis orbit of disk 1 to change from a crescent shape to a petal shape. This study offers theoretical insights and empirical data that may assist in the structural design and fault diagnosis of two-span three-support rotors.</p>https://ms.copernicus.org/articles/16/375/2025/ms-16-375-2025.pdf
spellingShingle Z. Zhou
G. Bin
C. Li
Y. Gao
M. Bayjid Md
Vibration responses of a two-span three-support rotor system with sliding bearing elevation change
Mechanical Sciences
title Vibration responses of a two-span three-support rotor system with sliding bearing elevation change
title_full Vibration responses of a two-span three-support rotor system with sliding bearing elevation change
title_fullStr Vibration responses of a two-span three-support rotor system with sliding bearing elevation change
title_full_unstemmed Vibration responses of a two-span three-support rotor system with sliding bearing elevation change
title_short Vibration responses of a two-span three-support rotor system with sliding bearing elevation change
title_sort vibration responses of a two span three support rotor system with sliding bearing elevation change
url https://ms.copernicus.org/articles/16/375/2025/ms-16-375-2025.pdf
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AT cli vibrationresponsesofatwospanthreesupportrotorsystemwithslidingbearingelevationchange
AT ygao vibrationresponsesofatwospanthreesupportrotorsystemwithslidingbearingelevationchange
AT mbayjidmd vibrationresponsesofatwospanthreesupportrotorsystemwithslidingbearingelevationchange