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Experimental study of centrifugal compressor vaneless diffuser width

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Abstract

Seven different vaneless diffuser designs for a centrifugal compressor, varying only in diffuser width, were studied experimentally. The studied diffuser widths versus impeller exit width were 1.0, 0.903, 0.854, and 0.806. Three of the narrowed diffusers had the width reduced from the hub and shroud divided evenly, and the three others had the width reduced only from the shroud. The total and static pressures, the total temperature and the flow angles at the diffuser inlet and outlet were measured at the design rotational speed with three different mass flows. The impeller and diffuser performance was studied along with the axial distributions of flow angles and velocities in the diffuser. The results revealed that the pinch improved the compressor stage and impeller performance but deteriorated the diffuser performance. The pinch clearly decreased the secondary flow region present near the shroud. The pinch implemented in the shroud is more beneficial than pinch divided between the hub and the shroud. In order to obtain the beneficial effects of pinch, the pinch should be sufficient. However, excessive pinch deteriorates the compressor performance.

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References

  1. Y. Senoo and Y. Kinoshita, Influence of inlet flow conditions and geometries of centrifugal vaneless diffusers on critical flow angle for reverse flow, Journal of Fluids Engineering, 99(1) (1977) 98–103.

    Article  Google Scholar 

  2. R. A. Van den Braembuscsche, P. Frigne and M. Roustan, Rotating non-uniform flow in radial compressors, AGARD 55thB Specialist meeting of PEP, 282, paper 12, May 7–9, Brussels, Belgium, (1980).

    Google Scholar 

  3. K. B. Abidogun, Effects of vaneless diffuser geometries on rotating stall, ASME 4th International Pipeline Conference, IPC2002-27203, September 29–October 3, Alberta, Canada (2002).

    Google Scholar 

  4. A. Engeda, Experimental and numerical investigation of the performance of a 240 kW centrifugal compressor with different diffusers, Experimental Thermal and Fluid Science, 28(1) (2003) 55–72.

    Article  Google Scholar 

  5. K. Ludtke, Aerodynamic tests on centrifugal process compressors — the influence of vaneless diffuser shape, Journal of Engineering for Power, 105(4) (1983) 902–909.

    Article  Google Scholar 

  6. G. Ferrara, L. Ferrari, C. P. Mengoni, M. D. Lucia and L. Baldassarre, Experimental investigation and characterization of rotating stall in a high pressure centrifugal compressor: Part I: Influence of diffuser geometry on stall inception, ASME Turbo Expo, GT2002-30389, June 3–6, Amsterdam, the Netherlands, (2002).

    Google Scholar 

  7. G. Ferrara, L. Ferrari, C. P. Mengoni, M. D. Lucia and L. Baldassarre, Experimental investigation and characterization of rotating stall in a high pressure centrifugal compressor: Part II: Influence of diffuser geometry on stage performance, ASME Turbo Expo, GT2002-30390, June 3–6, Amsterdam, the Netherlands, (2002).

    Google Scholar 

  8. A. Cellai, G. Ferrara, L. Ferrari, C. P. Mengoni and L. Baldassarre, Experimental investigation and characterization of rotating stall in a high pressure centrifugal compressor: Part III: Influence of diffuser geometry on stall inception and performance (2nd impeller tested), ASME Turbo Expo, GT2003-38390, June 16–19, Atlanta, Georgia, USA, (2003).

    Google Scholar 

  9. J. Tang, Computational analysis and optimization of real gas flow in small centrifugal compressors, Ph.D Dissertation, Institute of Energy, Lappeeranta University of Technology, Finland, (2006).

    Google Scholar 

  10. T. Turunen-Saaresti, A. Reunanen and J. Larjola, Computational and experimental study of pinch on the performance of a vaneless diffuser of a centrifugal compressor, Journal of Thermal Science, 15(4) (2006) 306–313.

    Article  Google Scholar 

  11. T. Turunen-Saaresti, A. Gronman and A. Jaatinen, Experimental study of pinch on the performance of a vaneless diffuser of a centrifugal compressor, ASME Turbo Expo, GT2009-60162, June 8–12, Orlando, Florida, USA, (2009).

    Google Scholar 

  12. A. Jaatinen, A. Gronman, T. Turunen-Saaresti and P. Roytta, Effect of vaneless diffuser width on the overall performance of a centrifugal compressor, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 225 (2011) 665–673.

    Article  Google Scholar 

  13. DIN 1952, Durchflußmessung mit genormten Dusen, Blenden und Venturdusen, Deutsches Institut fur Normung e.V. (1971).

  14. ASME PTC 10, ASME Power Test Codes, compressors and exhausters. The American Society of Mechanical Engineering, (1965).

  15. ISO 5389, Turbocompressors — Performance test code. International Standardization Organization, (1992).

    Google Scholar 

  16. VDI 2045 Part 1, Abnahme- und Leistungsversuche an Verdichtern, Versuchsdurchfuhrung und Garantievergleich (Acceptance and Performance Test on Turbo Compressors and Displacement Compressors, Test Procedure and Comparison with Guaranteed Values). Verein Deutscher Ingenieure, (1993).

  17. VDI 2045 Part 2, Abnahme- und Leistungversuche an Verdichtern, Grundlagen und Beispiele (Acceptance and Performance Test on Turbo Compressors and Displacement Compressors, Theroy and Examples). Verein Deutscher Ingenieure, (1993).

  18. T. Mashimo, I. Watanabe and I. Ariga, Effect of fluid leakage on performance of a centrifugal compressor, Journal of Engineering for Power, 101(3) (1979) 337–342.

    Article  Google Scholar 

  19. Y. Senoo and M. Ishida, Deterioration of compressor performance due to tip clearance of centrifugal impellers, Journal of Turbomachinery, 109(1) (1987) 55–61.

    Article  Google Scholar 

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Correspondence to Ahti Jaatinen-Värri.

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Recommended by Associate Editor Byeong Rog Shin

Ahti Jaatinen-Värri currently works as a post-doctoral researcher at the Laboratory of Fluid Dynamics, in Lappeenranta University of Technology, Finland. He received his doctoral degree from Lapeenranta University of Technolgy in 2009, majoring in fluid dynamics and heat transefer. His main areas of intrest are internal flows in various high-speed turbomachinery, especially centrifugal compressor aerodynamics.

Pekka Röyttä, born 1981, in Tornio, Finland. Dr. Roytta obtained his M.Sc. and D.Sc. degrees from Lappeenranta University of Technology (LUT) in 2006 and 2009, respectively. Currently acting as a post-doctoral researcher of Academy of Finland at LUT. His research interests include CFD — especially large eddy simulations, multi-physics simulations, turbomachinery, and heat transfer.

Teemu Turunen-Saaresti eanred his M.Sc. in 2001 and D.Sc in 2004 from Lappeenranta University of Technology, Finland. He currently works as an Academy research Fellow and associate professor in the Laboratory of Fluid Dynamics in Lappeenrata University of Technology.

Aki Grönman is a post-doctoral researcher at the Laboratory of Fluid Dynamics, Lappeenranta University of Technology, Finland. He received his doctoral degree from Lappeenranta University of Technology in 2010 from fluid mechanics and heat transfer. His research has been concentrated in axial turbine and centrifugal compressor aerodynamics and design.

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Jaatinen-Värri, A., Röyttä, P., Turunen-Saaresti, T. et al. Experimental study of centrifugal compressor vaneless diffuser width. J Mech Sci Technol 27, 1011–1020 (2013). https://doi.org/10.1007/s12206-013-0122-y

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  • DOI: https://doi.org/10.1007/s12206-013-0122-y

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