Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser

The effect of the width of the vaneless diffuser on the stage performance and flow fields of a centrifugal compressor is studied numerically and experimentally. The diffuser width is varied by reducing the diffuser flow area from the shroud side (i.e., pinching the diffuser). Seven different diffuse...

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Main Authors: Ahti Jaatinen-Värri, Aki Grönman, Teemu Turunen-Saaresti, Jari Backman
Format: Article
Language:English
Published: Hindawi Limited 2014-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/2014/139153
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spelling doaj-0336d229629f49408664033c19e756e52020-11-24T21:17:04ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X1542-30342014-01-01201410.1155/2014/139153139153Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless DiffuserAhti Jaatinen-Värri0Aki Grönman1Teemu Turunen-Saaresti2Jari Backman3Institute of Energy, Lappeenranta University of Technology, P.O. Box 20, 53851 Lappeenranta, FinlandInstitute of Energy, Lappeenranta University of Technology, P.O. Box 20, 53851 Lappeenranta, FinlandInstitute of Energy, Lappeenranta University of Technology, P.O. Box 20, 53851 Lappeenranta, FinlandInstitute of Energy, Lappeenranta University of Technology, P.O. Box 20, 53851 Lappeenranta, FinlandThe effect of the width of the vaneless diffuser on the stage performance and flow fields of a centrifugal compressor is studied numerically and experimentally. The diffuser width is varied by reducing the diffuser flow area from the shroud side (i.e., pinching the diffuser). Seven different diffuser widths are studied with numerical simulation. In the modeling, the diffuser width b/b2 is varied within the range 1.00 to 0.50. The numerical results are compared with results obtained in previous studies. In addition, two of the diffusers are further investigated with experimental measurement. The main finding of the work is that the pinch reduces losses in the impeller associated with the tip-clearance flow. Furthermore, it is shown that a too large width reduction causes the flow to accelerate excessively, resulting in a highly nonuniform flow field and flow separation near the shroud.http://dx.doi.org/10.1155/2014/139153
collection DOAJ
language English
format Article
sources DOAJ
author Ahti Jaatinen-Värri
Aki Grönman
Teemu Turunen-Saaresti
Jari Backman
spellingShingle Ahti Jaatinen-Värri
Aki Grönman
Teemu Turunen-Saaresti
Jari Backman
Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser
International Journal of Rotating Machinery
author_facet Ahti Jaatinen-Värri
Aki Grönman
Teemu Turunen-Saaresti
Jari Backman
author_sort Ahti Jaatinen-Värri
title Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser
title_short Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser
title_full Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser
title_fullStr Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser
title_full_unstemmed Investigation of the Stage Performance and Flow Fields in a Centrifugal Compressor with a Vaneless Diffuser
title_sort investigation of the stage performance and flow fields in a centrifugal compressor with a vaneless diffuser
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
1542-3034
publishDate 2014-01-01
description The effect of the width of the vaneless diffuser on the stage performance and flow fields of a centrifugal compressor is studied numerically and experimentally. The diffuser width is varied by reducing the diffuser flow area from the shroud side (i.e., pinching the diffuser). Seven different diffuser widths are studied with numerical simulation. In the modeling, the diffuser width b/b2 is varied within the range 1.00 to 0.50. The numerical results are compared with results obtained in previous studies. In addition, two of the diffusers are further investigated with experimental measurement. The main finding of the work is that the pinch reduces losses in the impeller associated with the tip-clearance flow. Furthermore, it is shown that a too large width reduction causes the flow to accelerate excessively, resulting in a highly nonuniform flow field and flow separation near the shroud.
url http://dx.doi.org/10.1155/2014/139153
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