Research on unbalance response characteristics of gas turbine blade-disk rotor system

Taken a gas turbine rotor system as the research object, this paper has established dynamical model based on transfer matrix method. Natural vibration characteristics are solved with different transfer matrix models, and are compared with that gotten by finite element method. Then unbalanced respons...

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Main Authors: Wenjun Yang, Mingxuan Liang, Lei Wang, Huiqun Yuan
Format: Article
Language:English
Published: JVE International 2018-06-01
Series:Journal of Vibroengineering
Subjects:
Online Access:https://www.jvejournals.com/article/18765
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spelling doaj-a707b710d1b44ce88afae9809dbea1962020-11-25T00:11:03ZengJVE InternationalJournal of Vibroengineering1392-87162538-84602018-06-012041676169010.21595/jve.2018.1876518765Research on unbalance response characteristics of gas turbine blade-disk rotor systemWenjun Yang0Mingxuan Liang1Lei Wang2Huiqun Yuan3School of Mechatronics Engineering, Shenyang Aerospace University, Shenyang, ChinaCollege of Mechanical and Electrical Engineering, China Jiliang University, Hangzhou, ChinaSchool of Mechatronics Engineering, Shenyang Aerospace University, Shenyang, ChinaSchool of Mechanical Engineering and Automation, Northeastern University, Shenyang, ChinaTaken a gas turbine rotor system as the research object, this paper has established dynamical model based on transfer matrix method. Natural vibration characteristics are solved with different transfer matrix models, and are compared with that gotten by finite element method. Then unbalanced response is researched. The effects of eccentric factors are discussed on unbalanced vibration. Furthermore, the application is explored in rotor dynamic balancing. The results show there is much minor deviation between natural frequencies of transfer matrix method and finite element method, and vibration modes of two methods coincide quite well. It illustrates the model established in the research is reliable. For input side of blade-disk rotor, unbalanced vibration occurs more easily in lower frequency. While unbalanced vibration of output side is more sensitive at higher frequency. With the increase of eccentric mass, unbalanced vibration of blade-disk rotor is more heavily, and the displacement rotates around a fixed node. The application of opposite unbalanced mass can decrease the amplitude of vibration in lower frequency. Hence, it can be used to achieve the balance of rotor dynamics. This research provides the theoretical basis and technological fundament for gas turbine rotor dynamics design.https://www.jvejournals.com/article/18765blade-disk rotortransfer matrix analysisdynamic characteristiceccentric factorunbalanced response
collection DOAJ
language English
format Article
sources DOAJ
author Wenjun Yang
Mingxuan Liang
Lei Wang
Huiqun Yuan
spellingShingle Wenjun Yang
Mingxuan Liang
Lei Wang
Huiqun Yuan
Research on unbalance response characteristics of gas turbine blade-disk rotor system
Journal of Vibroengineering
blade-disk rotor
transfer matrix analysis
dynamic characteristic
eccentric factor
unbalanced response
author_facet Wenjun Yang
Mingxuan Liang
Lei Wang
Huiqun Yuan
author_sort Wenjun Yang
title Research on unbalance response characteristics of gas turbine blade-disk rotor system
title_short Research on unbalance response characteristics of gas turbine blade-disk rotor system
title_full Research on unbalance response characteristics of gas turbine blade-disk rotor system
title_fullStr Research on unbalance response characteristics of gas turbine blade-disk rotor system
title_full_unstemmed Research on unbalance response characteristics of gas turbine blade-disk rotor system
title_sort research on unbalance response characteristics of gas turbine blade-disk rotor system
publisher JVE International
series Journal of Vibroengineering
issn 1392-8716
2538-8460
publishDate 2018-06-01
description Taken a gas turbine rotor system as the research object, this paper has established dynamical model based on transfer matrix method. Natural vibration characteristics are solved with different transfer matrix models, and are compared with that gotten by finite element method. Then unbalanced response is researched. The effects of eccentric factors are discussed on unbalanced vibration. Furthermore, the application is explored in rotor dynamic balancing. The results show there is much minor deviation between natural frequencies of transfer matrix method and finite element method, and vibration modes of two methods coincide quite well. It illustrates the model established in the research is reliable. For input side of blade-disk rotor, unbalanced vibration occurs more easily in lower frequency. While unbalanced vibration of output side is more sensitive at higher frequency. With the increase of eccentric mass, unbalanced vibration of blade-disk rotor is more heavily, and the displacement rotates around a fixed node. The application of opposite unbalanced mass can decrease the amplitude of vibration in lower frequency. Hence, it can be used to achieve the balance of rotor dynamics. This research provides the theoretical basis and technological fundament for gas turbine rotor dynamics design.
topic blade-disk rotor
transfer matrix analysis
dynamic characteristic
eccentric factor
unbalanced response
url https://www.jvejournals.com/article/18765
work_keys_str_mv AT wenjunyang researchonunbalanceresponsecharacteristicsofgasturbinebladediskrotorsystem
AT mingxuanliang researchonunbalanceresponsecharacteristicsofgasturbinebladediskrotorsystem
AT leiwang researchonunbalanceresponsecharacteristicsofgasturbinebladediskrotorsystem
AT huiqunyuan researchonunbalanceresponsecharacteristicsofgasturbinebladediskrotorsystem
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