Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior

The increased use of small gas turbines and turbochargers in different technical fields has led to the development of highly-loaded centrifugal compressors with extremely thin blades. Due to high rotational speed and the correspondingly high centrifugal loads, the shape of the impeller hub must also...

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Main Authors: Dirk Hagelstein, Heinrich Hasemann, Manfred Rautenberg
Format: Article
Language:English
Published: Wiley 2000-01-01
Series:International Journal of Rotating Machinery
Subjects:
Online Access:http://dx.doi.org/10.1155/S1023621X00000117
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author Dirk Hagelstein
Heinrich Hasemann
Manfred Rautenberg
author_facet Dirk Hagelstein
Heinrich Hasemann
Manfred Rautenberg
author_sort Dirk Hagelstein
collection DOAJ
description The increased use of small gas turbines and turbochargers in different technical fields has led to the development of highly-loaded centrifugal compressors with extremely thin blades. Due to high rotational speed and the correspondingly high centrifugal loads, the shape of the impeller hub must also be optimized. This has led to a reduction of the thickness of the impeller disc in the outlet region. The thin parts of the impeller are very sensitive and may be damaged by the excitation of dangerous blade vibrations.
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publishDate 2000-01-01
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series International Journal of Rotating Machinery
spelling doaj-art-82812d0eaa3e410d90f770b99c88e3d22025-02-03T05:48:14ZengWileyInternational Journal of Rotating Machinery1023-621X2000-01-016211512810.1155/S1023621X00000117Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration BehaviorDirk Hagelstein0Heinrich Hasemann1Manfred Rautenberg2Institute of Turbomachinery, University of Hannover, Appelstr. 9, Hannover D-30167, GermanyInstitute of Turbomachinery, University of Hannover, Appelstr. 9, Hannover D-30167, GermanyInstitute of Turbomachinery, University of Hannover, Appelstr. 9, Hannover D-30167, GermanyThe increased use of small gas turbines and turbochargers in different technical fields has led to the development of highly-loaded centrifugal compressors with extremely thin blades. Due to high rotational speed and the correspondingly high centrifugal loads, the shape of the impeller hub must also be optimized. This has led to a reduction of the thickness of the impeller disc in the outlet region. The thin parts of the impeller are very sensitive and may be damaged by the excitation of dangerous blade vibrations.http://dx.doi.org/10.1155/S1023621X00000117Centrifugal compressorBlade vibrationsCoupled vibrationsFinite element computation.
spellingShingle Dirk Hagelstein
Heinrich Hasemann
Manfred Rautenberg
Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
International Journal of Rotating Machinery
Centrifugal compressor
Blade vibrations
Coupled vibrations
Finite element computation.
title Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
title_full Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
title_fullStr Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
title_full_unstemmed Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
title_short Coupled Vibration of Unshrouded Centrifugal Compressor Impellers. Part II: Computation of Vibration Behavior
title_sort coupled vibration of unshrouded centrifugal compressor impellers part ii computation of vibration behavior
topic Centrifugal compressor
Blade vibrations
Coupled vibrations
Finite element computation.
url http://dx.doi.org/10.1155/S1023621X00000117
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