CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR

A type of aero engine compressor blade model was built based on finite element. Dynamics of the clamped constrained blade was obtained by modal simulation and the influence of centrifugal force on the vibration of blades was researched. And then,the modal test was carried out to validate the model a...

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Main Authors: YIN ZhiPeng, LI QuanTong, GAO XingWei, CHEN PengFei, TANG Ling
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2016-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.03.005
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author YIN ZhiPeng
LI QuanTong
GAO XingWei
CHEN PengFei
TANG Ling
author_facet YIN ZhiPeng
LI QuanTong
GAO XingWei
CHEN PengFei
TANG Ling
author_sort YIN ZhiPeng
collection DOAJ
description A type of aero engine compressor blade model was built based on finite element. Dynamics of the clamped constrained blade was obtained by modal simulation and the influence of centrifugal force on the vibration of blades was researched. And then,the modal test was carried out to validate the model and the simulation data. Vibration analysis of blade disc finite element model was carried out based on cyclic symmetry method. The vibration mode and frequency of the coupling system with different working speeds were obtained. The result shows that the natural frequency of the coupling system is lower in the same order when compared with a single fixed blade. The resonance frequency and the corresponding rotor speed could be obtained by analysis of Campbell contours. It provides reference for the fault diagnosis,reliability analysis and life estimation.
format Article
id doaj-art-28398b99fae24d408d1bf6ba54a121b1
institution Kabale University
issn 1001-9669
language zho
publishDate 2016-01-01
publisher Editorial Office of Journal of Mechanical Strength
record_format Article
series Jixie qiangdu
spelling doaj-art-28398b99fae24d408d1bf6ba54a121b12025-01-15T02:36:25ZzhoEditorial Office of Journal of Mechanical StrengthJixie qiangdu1001-96692016-01-013845345830594886CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSORYIN ZhiPengLI QuanTongGAO XingWeiCHEN PengFeiTANG LingA type of aero engine compressor blade model was built based on finite element. Dynamics of the clamped constrained blade was obtained by modal simulation and the influence of centrifugal force on the vibration of blades was researched. And then,the modal test was carried out to validate the model and the simulation data. Vibration analysis of blade disc finite element model was carried out based on cyclic symmetry method. The vibration mode and frequency of the coupling system with different working speeds were obtained. The result shows that the natural frequency of the coupling system is lower in the same order when compared with a single fixed blade. The resonance frequency and the corresponding rotor speed could be obtained by analysis of Campbell contours. It provides reference for the fault diagnosis,reliability analysis and life estimation.http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.03.005Compressor bladeBlade-disc couplingVibration characteristicsFinite element
spellingShingle YIN ZhiPeng
LI QuanTong
GAO XingWei
CHEN PengFei
TANG Ling
CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
Jixie qiangdu
Compressor blade
Blade-disc coupling
Vibration characteristics
Finite element
title CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
title_full CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
title_fullStr CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
title_full_unstemmed CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
title_short CALCULATION OF THE BLADE AND THE BLADE-DISC COUPLING SYSTEM OF COMPRESSOR
title_sort calculation of the blade and the blade disc coupling system of compressor
topic Compressor blade
Blade-disc coupling
Vibration characteristics
Finite element
url http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2016.03.005
work_keys_str_mv AT yinzhipeng calculationofthebladeandthebladedisccouplingsystemofcompressor
AT liquantong calculationofthebladeandthebladedisccouplingsystemofcompressor
AT gaoxingwei calculationofthebladeandthebladedisccouplingsystemofcompressor
AT chenpengfei calculationofthebladeandthebladedisccouplingsystemofcompressor
AT tangling calculationofthebladeandthebladedisccouplingsystemofcompressor