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Performance Optimization of Centrifugal Compressors Based on Throughflow Model

  • Research Article-Mechanical Engineering
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Abstract

In order to realize the fast performance analysis of centrifugal compressor, the performance calculation program of centrifugal compressor based on time marching throughflow method was developed. On this basis, combined with blade parameterization method and multi-objective genetic algorithm, the aerodynamic performance of LSCC and Krain centrifugal compressor was optimized with efficiency and pressure ratio as optimization objectives on design point. The results show that, compared with the prototype, the efficiency of LSCC compressor at design point was increased by 0.28\(\%\), the total pressure ratio was improved by 0.551\(\%\), and its stable working range was widened furtherly; the efficiency of Krain compressor at design point was increased by 0.518\(\%\); the total pressure ratio was improved by 2.27\(\%\); at the same time, the effectiveness of the performance optimization method was verified.

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References

  1. Holland, J.H.: Adaptation in Natural and Artificial Systems: An Introductory Analysis with Applications to Biology, Control, and Artificial Intelligence. MIT Press (1992)

  2. Deb, K.; Agrawal, S.; et al.: A fast elitist non-dominated sorting genetic algorithm for multi-objective optimization: NSGA-II. Lect. Notes Comput. Sci. 1917, 849–858 (2000)

    Article  Google Scholar 

  3. Yamaguchi, Y.; Arima, T.: Multi-objective optimization for the transonic compressor stator blade. Symposium on Multidisciplinary Analysis & Optimization (2000)

  4. Hildebrandt, A.: Aerodynamic optimization of a centrifugal compressor return channel and u-turn with genetic algorithms. Asme Turbo Expo: Turbine Technical Conference & Exposition (2011)

  5. Liu, X.; Zhang, W.: Two schemes of multi-objective aerodynamic optimization for centrifugal impeller using response surface model and genetic algorithm. Asme Turbo Expo: Power for Land, Sea, & Air (2010)

  6. Bing, X.; Yang, C.X.: The use of a genetic algorithm for the structure optimization of a centrifugal compressor impeller. J. Eng. Therm. Energy Power 16(2):182–185 (2001)

  7. Myoren, C.; Takahashi, Y.; Kato, Y.: Multi-objective optimization of three-dimensional blade shape for an axial compressor rotor in transonic stage. Int. J. Gas Turbine Propul. Power Syst. 5(1): 8–16 (2013)

  8. Wei, D.: Aerodynamic optimization design of axial compressor based on multi objective genetic algorithm. Northwestern Polytechnical University (2006)

  9. Zhao, L.Z.; Qing Hua, D.; Feng, Z.P.: Aerodynamic optimization design of vaned diffuser for centrifugal compressor under stage environment. J. Xi’an Jiaotong Univ. 43(11), 32–36 (2009)

    Google Scholar 

  10. Ivanov, M.J.: Mathematical Models of Gas Turbine Engines and their components. AGARD LS-198, AGARD publications (1994)

  11. Simon, J.F.; Léonard, O.: Modeling of 3-D losses and deviations in a throughflow analysis tool. J. Therm. Sci. 16(3), 208–214 (2007)

    Article  Google Scholar 

  12. Yang, C.; Wu, H.; Yang, et al.: Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model. Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. (2019)

  13. Qiu et al.: A new slip factor model for axial and radial impellers. ASME Turbo Expo 2007: Power for Land, Sea, and Air (2007)

  14. Yoon, S.; Jameson, A.: Lower-upper symmetric-gaussseidel method for the Euler and Navier–Stokes equations. AIAA J. (1988)

  15. Aungier, R.H.: Mean streamline aerodynamic performance analysis of centrifugal compressors. J. Turbomach. 117(3), 1 (1995)

    Article  Google Scholar 

  16. Coppage et al.: Study of supersonic radial compressors for refrigeration and pressurization systems (1956)

  17. Jansen, W.: A method for calculating the flow in a centrifugal impeller when entropy gradient are present. Inst. Mech. Eng. Internal Aerodyn. (1970)

  18. Johnston, J.P.; Dean, R.C.: Losses in vaneless diffusers of centrifugal compressors and pumps: analysis, experiment, and design. 88(1):49 (1966)

  19. Daily, J.W.; Nece, R.E.: Chamber dimension effects on induced flow and frictional resistance of enclosed rotating disks. 82(1), 217 (1960)

  20. Yang et al.: Improved performance model of turbocharger centrifugal compressor. ASME Turbo Expo: Power for Land, Sea, and Air.vol. 43161:1439–1445 (2008)

  21. Hathaway, Michael D.; Chriss, Randall M.; et al.: Experimental and computational investigation of the NASA low-speed centrifugal compressor flow field. (1992)

  22. Hathaway, M.D.; Chriss, R.M.; et al.: Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor (1995)

  23. Chriss, R.M.; Wood, J.R.; Hathaway, M.D.: Experimental and computational results from the NASA Lewis low-speed centrifugal impeller at design and part-flow conditions. J. Turbomach. 118(1), 1 (1996)

    Article  Google Scholar 

  24. Krain, H.: Swirling impeller flow. (1988)

  25. Skoch, G.J.; Prahst, P.S.; et al.: Laser anemometer measurements of the flow field in a 4: 1 pressure ratio centrifugal impeller. Am. Soc. Mech. Eng. (1997)

  26. Hah, C.; Krain, H.: Secondary flows and vortex motion in a high-efficiency backswept impeller at design and off-design conditions. J. Turbomach. ASME Pap. 1989, 1–10 (1990)

  27. Clayton, R.P.; Leong, W.U.A.; et al.: A numerical study of the three-dimensional turbulent flow in the impeller of a high-speed centrifugal compressor. Turbo Expo: Power for Land, Sea, and Air: vol. 78620. American Society of Mechanical Engineers: V001T01A017 (1998)

  28. Sun, Z.: Investigation on the flow features and flowfield structures of centrifugal compressors. Inst. Eng. Thermophys. (2011)

  29. Jameson, A.; Schmidt, W.; Turkel, E.: Numerical solutions of the euler equations by finite volume methods using runge-kutta time-stepping schemes. In: AIAA 14th Fluid and Plasma Dynamics Conference (1981)

  30. Spalart, P. R.; Allmaras, S. R.: A one-equation turbulence model for aerodynamic flows. Recherche Aerospatiale (1992)

  31. Yu, R.B.: Genetic algorithm based blade profile aerodynamic optimal design. Equipm. Manuf. Technol. 01, 64–65 (2014)

    Google Scholar 

  32. Yuyang, L.; Xin, J.: Parameter optimization theory and examples of isight. Beihang University Press (2012)

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Acknowledgements

The first author would like to thank Professor H. Wu for providing many references on the CFD applications of their research achievements. The authors are grateful to Dr C. Yang for the help of throughflow model.

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Correspondence to Hu Wu.

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Tang, Q., Wu, H., Li, J. et al. Performance Optimization of Centrifugal Compressors Based on Throughflow Model. Arab J Sci Eng 47, 16439–16450 (2022). https://doi.org/10.1007/s13369-022-06736-2

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  • DOI: https://doi.org/10.1007/s13369-022-06736-2

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