Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces

In this paper, a synchronous vibration control method was proposed to avoid the high-cycle fatigue fracture of aeroengine rotor blade. Firstly. The harmonic force, causing synchronous vibration, was derived by Fourier series expansion by the mean of simplifying the aerodynamic exciting forces into t...

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Autores principales: Sanqun Ren, Xiaorong Xiang, Qingjun Zhao, Weimin Wang, Wei Zhao, Long Hao
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Lenguaje:EN
Publicado: SAGE Publishing 2021
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Acceso en línea:https://doaj.org/article/ce6e38f635ab43808d47d9fe8963b95f
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spelling oai:doaj.org-article:ce6e38f635ab43808d47d9fe8963b95f2021-12-02T01:34:54ZResearch on active control method of rotor blade synchronous vibration based on additional secondary excitation forces1461-34842048-404610.1177/14613484211008115https://doaj.org/article/ce6e38f635ab43808d47d9fe8963b95f2021-12-01T00:00:00Zhttps://doi.org/10.1177/14613484211008115https://doaj.org/toc/1461-3484https://doaj.org/toc/2048-4046In this paper, a synchronous vibration control method was proposed to avoid the high-cycle fatigue fracture of aeroengine rotor blade. Firstly. The harmonic force, causing synchronous vibration, was derived by Fourier series expansion by the mean of simplifying the aerodynamic exciting forces into the periodic rectangular pulse wave forces. It was found that the synchronous vibration can be controlled by adjusting the primary excitation forces parameters. Based on this, the additional secondary excitation forces were introduced to control the synchronous vibration caused by primary excitation forces. Secondly, the influences of the number, position, direction, duration of additional secondary excitation forces and the phase difference between additional secondary excitation forces and primary excitation forces on the synchronous vibration control were obtained through theoretical analysis, which was simulated and verified by a single-degree-of-freedom model. Thirdly, a high-speed straight blade test bench was established, and the feasibility of the method in controlling synchronous vibration of rotor blade was proved by adding additional magnet excitation forces on the basis of fixed magnet excitation forces. Finally, the suppression strategy of synchronous vibration of rotor blade by introducing additional secondary excitation forces was given. It can provide theoretical and technical support for effectively controlling the synchronous vibration amplitude and avoiding the high-cycle fatigue fracture of rotor blade in engineering practice.Sanqun RenXiaorong XiangQingjun ZhaoWeimin WangWei ZhaoLong HaoSAGE PublishingarticleControl engineering systems. Automatic machinery (General)TJ212-225Acoustics. SoundQC221-246ENJournal of Low Frequency Noise, Vibration and Active Control, Vol 40 (2021)
institution DOAJ
collection DOAJ
language EN
topic Control engineering systems. Automatic machinery (General)
TJ212-225
Acoustics. Sound
QC221-246
spellingShingle Control engineering systems. Automatic machinery (General)
TJ212-225
Acoustics. Sound
QC221-246
Sanqun Ren
Xiaorong Xiang
Qingjun Zhao
Weimin Wang
Wei Zhao
Long Hao
Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
description In this paper, a synchronous vibration control method was proposed to avoid the high-cycle fatigue fracture of aeroengine rotor blade. Firstly. The harmonic force, causing synchronous vibration, was derived by Fourier series expansion by the mean of simplifying the aerodynamic exciting forces into the periodic rectangular pulse wave forces. It was found that the synchronous vibration can be controlled by adjusting the primary excitation forces parameters. Based on this, the additional secondary excitation forces were introduced to control the synchronous vibration caused by primary excitation forces. Secondly, the influences of the number, position, direction, duration of additional secondary excitation forces and the phase difference between additional secondary excitation forces and primary excitation forces on the synchronous vibration control were obtained through theoretical analysis, which was simulated and verified by a single-degree-of-freedom model. Thirdly, a high-speed straight blade test bench was established, and the feasibility of the method in controlling synchronous vibration of rotor blade was proved by adding additional magnet excitation forces on the basis of fixed magnet excitation forces. Finally, the suppression strategy of synchronous vibration of rotor blade by introducing additional secondary excitation forces was given. It can provide theoretical and technical support for effectively controlling the synchronous vibration amplitude and avoiding the high-cycle fatigue fracture of rotor blade in engineering practice.
format article
author Sanqun Ren
Xiaorong Xiang
Qingjun Zhao
Weimin Wang
Wei Zhao
Long Hao
author_facet Sanqun Ren
Xiaorong Xiang
Qingjun Zhao
Weimin Wang
Wei Zhao
Long Hao
author_sort Sanqun Ren
title Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
title_short Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
title_full Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
title_fullStr Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
title_full_unstemmed Research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
title_sort research on active control method of rotor blade synchronous vibration based on additional secondary excitation forces
publisher SAGE Publishing
publishDate 2021
url https://doaj.org/article/ce6e38f635ab43808d47d9fe8963b95f
work_keys_str_mv AT sanqunren researchonactivecontrolmethodofrotorbladesynchronousvibrationbasedonadditionalsecondaryexcitationforces
AT xiaorongxiang researchonactivecontrolmethodofrotorbladesynchronousvibrationbasedonadditionalsecondaryexcitationforces
AT qingjunzhao researchonactivecontrolmethodofrotorbladesynchronousvibrationbasedonadditionalsecondaryexcitationforces
AT weiminwang researchonactivecontrolmethodofrotorbladesynchronousvibrationbasedonadditionalsecondaryexcitationforces
AT weizhao researchonactivecontrolmethodofrotorbladesynchronousvibrationbasedonadditionalsecondaryexcitationforces
AT longhao researchonactivecontrolmethodofrotorbladesynchronousvibrationbasedonadditionalsecondaryexcitationforces
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