In this paper the effect of the tip clearance was studied with six different centrifugal compressors and data available in literature. The changes in the overall performance of the compressor stage were examined. The aim was to study the influence of the different design parameters to the tip clearance loss. It was evident by the previous studies that the sensitivity of the centrifugal compressor to the tip clearance loss varies with different designs. However, for the designer it is important to know the effect of the tip clearance loss in order to initially evaluate the quality of different designs. Analysis of the data demonstrated that no clear correlation between the sensitivity of the tip clearance loss and the specific speed, the diffusion ratio, the blade number and the ratio of blade heights exists.
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January 2013
Research-Article
Influence of the Different Design Parameters to the Centrifugal Compressor Tip Clearance Loss
Teemu Turunen-Saaresti,
Teemu Turunen-Saaresti
1
e-mail: teemu.turunen-saaresti@lut.fi
e-mail: ahti.jaatinen@lut.fi
Laboratory of Fluid Dynamics,
Lappeenranta University of Technology,
Laboratory of Fluid Dynamics,
Institute of Energy Technology
,Lappeenranta University of Technology,
Lappeenranta
, Finland
1Corresponding author.
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Ahti Jaatinen
Ahti Jaatinen
e-mail: ahti.jaatinen@lut.fi
Laboratory of Fluid Dynamics,
Lappeenranta University of Technology,
Laboratory of Fluid Dynamics,
Institute of Energy Technology
,Lappeenranta University of Technology,
Lappeenranta
, Finland
Search for other works by this author on:
Teemu Turunen-Saaresti
e-mail: teemu.turunen-saaresti@lut.fi
e-mail: ahti.jaatinen@lut.fi
Laboratory of Fluid Dynamics,
Lappeenranta University of Technology,
Laboratory of Fluid Dynamics,
Institute of Energy Technology
,Lappeenranta University of Technology,
Lappeenranta
, Finland
Ahti Jaatinen
e-mail: ahti.jaatinen@lut.fi
Laboratory of Fluid Dynamics,
Lappeenranta University of Technology,
Laboratory of Fluid Dynamics,
Institute of Energy Technology
,Lappeenranta University of Technology,
Lappeenranta
, Finland
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) Division of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received July 10, 2011; final manuscript received August 16, 2011; published online October 30, 2012. Editor: David Wisler.
J. Turbomach. Jan 2013, 135(1): 011017 (6 pages)
Published Online: October 30, 2012
Article history
Received:
July 10, 2011
Revision Received:
August 16, 2011
Citation
Turunen-Saaresti, T., and Jaatinen, A. (October 30, 2012). "Influence of the Different Design Parameters to the Centrifugal Compressor Tip Clearance Loss." ASME. J. Turbomach. January 2013; 135(1): 011017. https://doi.org/10.1115/1.4006388
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