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Influence of volute distortion on the performance of turbocharger centrifugal compressor with vane diffuser

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Abstract

As the geometry of the volute of turbocharger compressor is non-axisymmetric, it causes a distortion at the outlet of the diffuser and influences the upstream components. A distortion model in which a pressure distortion was applied as outlet boundary condition was established to simulate the distortion induced by the volute. It turned out to be sufficient to impose a circumferentially asymmetric pressure distribution at the outlet of the diffuser to replace the volute. Based on the distortion model which was verified, the influence of the amplitude of the distortion on the performance of centrifugal compressor was studied in detail. The results show that the distortion severely harms aerodynamic stability of the investigated compressor. The larger the amplitude of the distortion, the worse the performance of the compressor. The distortion induced by asymmetric volute propagates to upstream components and causes local flow separation at part of diffuser and impeller, and then causes the compressor surge. When the amplitude of the volute distortion is 10%, the stable flow range of the centrifugal compressor decreases to near zero. To authors’ knowledge, the relationship between the compressor performance and distortion amplitude is first obtained quantitatively, which provides evidence to improve the performance of turbocharger compressor by decreasing the distortion induced by asymmetric volute.

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Abbreviations

A :

amplitude of distortion

\(\dot m\) :

mass flow rate (kg s−1)

N :

rotating speed (r min−1)

PR :

pressure ratio

R2:

radius of the impeller (mm)

SFR :

stable flow range

η :

efficiency

References

  1. Ricardo M B, Apostolos P, Yang M Y. Overview of boosting options for future downsized engine. Sci China Tech Sci, 2011, 54(2): 318–331

    Article  Google Scholar 

  2. Lake T, Stokes J, Murphy R. Turbocharging concepts for downsized DI gasoline engines. SAE Paper No. 01-0036, 2004

    Google Scholar 

  3. Clenci A C, Descombes G, Podevin P, et al. Some aspects concerning the combination of downsizing with turbocharging, variable compression ratio, and variable intake valve lift. Proc Inst Mech Eng, Part D-J Automob Eng, 2007, 221(10): 1287–1294

    Article  Google Scholar 

  4. Zheng X Q, Zhang Y J, Yang M Y. Research and development on transonic compressor of high pressure ratio turbocharger for vehicle internal combustion engines. Sci China Tech Sci, 2010, 53(7): 1817–1823

    Article  MathSciNet  Google Scholar 

  5. Maiboom A, Tauzia X, Héteta J F. Experimental study of various effects of exhaust gas recirculation (EGR) on combustion and emissions of an automotive direct injection diesel engine. Energy, 2008, 33(1): 22–34

    Article  Google Scholar 

  6. Yu G, Ohashi K, Uchiyama Y. Influence of environmental conditions on diesel engine performance. SAE Paper No. 891347, 1989

    Google Scholar 

  7. Rodgers C. Turbocharging a high altitude UAV C.I. engine. AIAA Paper No. 3970, 2001

    Google Scholar 

  8. Jiao K, Sun H, Li X, et al. Numerical simulation of air flow through turbocharger compressors with dual volute design. Appl Energy, 2009, 86: 2494–2506

    Article  Google Scholar 

  9. Hillewaert K, Braembussche R V. Numerical simulation of impeller-volute interaction in centrifugal compressors. J Turbomach-Trans ASME, 1999, 121(3): 603–608

    Article  Google Scholar 

  10. Reunanen A, Pitkanen H, Larjola J, et al. Computational and experimental comparison of different volute geometries in a radial compressor. ASME Paper No. GT-469, 2000

    Google Scholar 

  11. Hagelstein D, Braembussche R V, Keiper R, et al. Experimental investigation of the circumferential static pressure distortion in centrifugal compressor stages. ASME Paper No. GT-50, 1997

    Google Scholar 

  12. Xu C, Amano R S. Eliminating static pressure distortion by a large cut back tongue volute. ASME Paper No. GT2006-90001, 2006

    Google Scholar 

  13. Yang M Y, Zheng X Q, Zhang Y J, et al. Stability improvement of high-pressure ratio turbocharger centrifugal compressor by asymmetric flow control-part I: non-axisymmetric flow in centrifugal compressor. ASME Paper No. GT2010-22581, 2010

    Google Scholar 

  14. Fatsis A, Pierret S, Braembussche R V. Three-dimensional unsteady flow and forces in centrifugal impellers with circumferential distortion of the oulet static pressure. J Turbomach-Trans ASME, 1997, 119(1): 94–102

    Article  Google Scholar 

  15. Gu F, Engeda A. A numerical investigation on the volute/impeller steady-state interaction due to circumferential distortion. ASME Paper No. GT-0328, 2001

    Google Scholar 

  16. Gu F, Engeda A, Cave M, et al. A numerical investigation on the volute/diffuser interaction due to the axial distortion at the impeller exit. J Fluids Eng-Trans ASME, 2001, 123(3): 475–483

    Article  Google Scholar 

  17. Dickmann H P, Thomas S W, Szwedowicz J, et al. Unsteady flow in a turbocharger centrifugal compressor: three-dimensional computational fluid dynamics simulation and numerical and experimental analysis of impeller blade vibration. J Turbomach-Trans ASME, 2006, 128(3): 455–465

    Article  Google Scholar 

  18. Zheng X Q, Huenteler J, Yang M Y, et al. Influence of the volute on the flow in a centrifugal compressor of a high-pressure ratio turbocharger. Proc Inst Mech Eng Part A-J Power Energy, 2010, 224: 1157–1169

    Article  Google Scholar 

  19. Lin Y, Zheng X Q, Jin L, et al. A novel experimental method to evaluate the impact of volute’s asymmetry on the performance of a high pressure ratio turbocharger compressor. Sci China Tech Sci, 2012, 55(6):1695–1700

    Article  Google Scholar 

  20. Jameson A, Baker T. Solutions of the Euler equations for complex configurations. AIAA Paper No. 1929, 1983

    Google Scholar 

  21. Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes. AIAA Paper No. 1259, 1981

    Google Scholar 

  22. Shaaban S, Seume J. Aerodynamic performance of small turbocharger compressors. ASME Paper No. GT2007-27558, 2007

    Google Scholar 

  23. Zheng X Q, Lin Y, Zhuge W L, et al. Stability improvement of turbocharger centrifugal compressor by asymmetric vaneless diffuser treatment. ASME Paper No. GT2013-94705, 2013

    Google Scholar 

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Correspondence to XinQian Zheng.

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Zheng, X., Jin, L. & Tamaki, H. Influence of volute distortion on the performance of turbocharger centrifugal compressor with vane diffuser. Sci. China Technol. Sci. 56, 2778–2786 (2013). https://doi.org/10.1007/s11431-013-5326-y

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  • DOI: https://doi.org/10.1007/s11431-013-5326-y

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