Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique
The arrangement optimization algorithm of blades can reduce the vibration localization of mistuned bladed disk in a compressor of aero-engine, however, it will destroy the dynamic balance of bladed disk. A new arrangement optimization method of isolation zone on bladed disk system considering unbala...
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doaj-8e03cd55103b4a5d80f7568fa08a77662021-04-01T19:07:01ZengJVE InternationalJournal of Vibroengineering1392-87162538-84602020-12-0123238539910.21595/jve.2020.2138121381Vibration reduction optimization for mistuned bladed disk based on reduced order modeling techniqueHongyuan Zhang0Huiqun Yuan1Hongyun Sun2School of Automotive and Transportation, Shenyang Ligong University, Shenyang, ChinaSchool of Mechanical Engineering and Automation, Northeastern University, Shenyang, ChinaSchool of Mechanical Engineering and Automation, Northeastern University, Shenyang, ChinaThe arrangement optimization algorithm of blades can reduce the vibration localization of mistuned bladed disk in a compressor of aero-engine, however, it will destroy the dynamic balance of bladed disk. A new arrangement optimization method of isolation zone on bladed disk system considering unbalance moment is proposed, on the basis the reduced order modeling technology. This method is based on the finite element model and can be implemented as fast and accurate vibration reduction optimization without destroying the mass balance of the bladed disk system, the method considers both mass and stiffness mistuning. Firstly, the discrete particle swarm optimization algorithm is used to sort the mass-mistuned blades according to unbalanced moment, then, the arranged bladed disk is divided into 6 isolation zones, then, in each isolation zone, the stiffness mistuned bladed disk is arranged optimally by the stiffness mistuning optimization algorithm. Under the premise of satisfying the dynamic balance of bladed disk, this algorithm optimizes the arrangement of blades with mass mistuning and stiffness mistuning, and achieves the purpose of vibration reduction optimization of mistuned bladed disk. The results show that, the maximum amplitude of the bladed disk system is reduced by 23.9 %. The vibration localization degree of the optimized blade are reduced by 46.3 %.https://www.jvejournals.com/article/21381mistuned bladed diskdiscrete particle swarmarrangement optimizationvibration reductionisolation zone |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Hongyuan Zhang Huiqun Yuan Hongyun Sun |
spellingShingle |
Hongyuan Zhang Huiqun Yuan Hongyun Sun Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique Journal of Vibroengineering mistuned bladed disk discrete particle swarm arrangement optimization vibration reduction isolation zone |
author_facet |
Hongyuan Zhang Huiqun Yuan Hongyun Sun |
author_sort |
Hongyuan Zhang |
title |
Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique |
title_short |
Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique |
title_full |
Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique |
title_fullStr |
Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique |
title_full_unstemmed |
Vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique |
title_sort |
vibration reduction optimization for mistuned bladed disk based on reduced order modeling technique |
publisher |
JVE International |
series |
Journal of Vibroengineering |
issn |
1392-8716 2538-8460 |
publishDate |
2020-12-01 |
description |
The arrangement optimization algorithm of blades can reduce the vibration localization of mistuned bladed disk in a compressor of aero-engine, however, it will destroy the dynamic balance of bladed disk. A new arrangement optimization method of isolation zone on bladed disk system considering unbalance moment is proposed, on the basis the reduced order modeling technology. This method is based on the finite element model and can be implemented as fast and accurate vibration reduction optimization without destroying the mass balance of the bladed disk system, the method considers both mass and stiffness mistuning. Firstly, the discrete particle swarm optimization algorithm is used to sort the mass-mistuned blades according to unbalanced moment, then, the arranged bladed disk is divided into 6 isolation zones, then, in each isolation zone, the stiffness mistuned bladed disk is arranged optimally by the stiffness mistuning optimization algorithm. Under the premise of satisfying the dynamic balance of bladed disk, this algorithm optimizes the arrangement of blades with mass mistuning and stiffness mistuning, and achieves the purpose of vibration reduction optimization of mistuned bladed disk. The results show that, the maximum amplitude of the bladed disk system is reduced by 23.9 %. The vibration localization degree of the optimized blade are reduced by 46.3 %. |
topic |
mistuned bladed disk discrete particle swarm arrangement optimization vibration reduction isolation zone |
url |
https://www.jvejournals.com/article/21381 |
work_keys_str_mv |
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