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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Main Authors: Hongyuan Zhang, Huiqun Yuan, Hongyun Sun
Format: Article
Language:English
Published: JVE International 2020-12-01
Series:Journal of Vibroengineering
Subjects:
Online Access:https://www.jvejournals.com/article/21381
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spelling 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 AT hongyuanzhang vibrationreductionoptimizationformistunedbladeddiskbasedonreducedordermodelingtechnique
AT huiqunyuan vibrationreductionoptimizationformistunedbladeddiskbasedonreducedordermodelingtechnique
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