American Journal of Energy Research
ISSN (Print): 2328-7349 ISSN (Online): 2328-7330 Website: https://www.sciepub.com/journal/ajer Editor-in-chief: Apply for this position
Open Access
Journal Browser
Go
American Journal of Energy Research. 2015, 3(2), 37-48
DOI: 10.12691/ajer-3-2-4
Open AccessArticle

Techno-Economic Optimization of Diffuser Configuration Effect on Centrifugal Compressor Performance

Waleed Al-Busaidi1, and Pericles Pilidis2

1Researcher in Cranfield University, Bedford, UK

2Head of Propulsion Engineering Centre, Cranfield University, Bedford, UK

Pub. Date: January 16, 2016

Cite this paper:
Waleed Al-Busaidi and Pericles Pilidis. Techno-Economic Optimization of Diffuser Configuration Effect on Centrifugal Compressor Performance. American Journal of Energy Research. 2015; 3(2):37-48. doi: 10.12691/ajer-3-2-4

Abstract

Extensive research has been conducted on centrifugal compressors to investigate the influence of diffuser features on the stage performance. However, there are several geometrical parameters affecting the diffuser performance and the unsteady interaction with the rotating impeller which makes the appropriate selection of the optimum features more complex. Furthermore, the trade-off between the efficiency improvement and operating range extension necessitates the need for an optimization tool to decide the typical diffuser configuration. Hence, this paper aims to introduce a multi-decision optimization approach to define the overall diffuser characteristics based on the specified duty requirements. This approach uses the most recent developed models in this field to evaluate the impact of different diffuser types on the overall stage performance technically and economically. From the performance perspective, the influences of diffuser geometry have been utilized to study the impact on stage efficiency and stable flow range. Furthermore, this has been also discussed economically as a function of the diffuser losses cost in order to make the typical decision.

Keywords:
centrifugal compressor diffuser characteristics optimization multi-decision process

Creative CommonsThis work is licensed under a Creative Commons Attribution 4.0 International License. To view a copy of this license, visit http://creativecommons.org/licenses/by/4.0/

References:

[1]  L. F. Schumann, (1985), A Three-Dimensional Axisymmetric Calculation Procedure for Turbulent Flows in a Radial Vaneless Diffuser, Paper No. 85-GT-133, ASME, New York.
 
[2]  Yingkang, Z. and Sjolander, S. (1987), Effects of Geometry on the Performance of Radial Vaneless Diffuser, Journal of Turbomachinery, 109:550-556.
 
[3]  Aungier, R. H. (1988), A Performance Analysis For The Vaneless Components Of Centrifugal Compressors, Flows In Non-Rotating Turbomachinery Components, ASME FED-Vol 69, 1988, pp. 35-43.
 
[4]  Y. Tsujimoto, Y. Yoshida, and Y. Mori (1996), Study of Vaneless Diffuser Rotating Stall Based on Two-Dimensional Inviscid Flow Analysis, Journal of Fluids Engineering, vol. 118, no. 1, pp. 123-127, 1996.
 
[5]  H. S. Dou and S. Mizuki (1996), Analysis of the Flow in Vaneless Diffusers with Large Width-to-Radius Ratios. In ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition (pp. V001T01A098-V001T01A098). American Society of Mechanical Engineers.
 
[6]  Yu-Tai Lee, Lin Luo and Thomas W. Bein (2001), Direct method for optimization of a centrifugal compressor vaneless diffuser, New York, ASME/2000-GT-453.
 
[7]  S. Ljevar, H. C. de Lange and A. A. Van Steenhoven (2006), Vaneless diffuser core flow instability and rotating stall characteristics. In Institution of Mechanical Engineers, Fluid Machinery Group-Ninth European Fluid Machinery Congress. UK: Institution of Me-chanical Engineers (pp. 379-389).
 
[8]  C. Gao, C. Gu, T. Wang, and Z. Dai (2008), Numerical analysis of rotating stall characteristics in vaneless diffuser with large width-radius ratio, Frontiers of Energy and Power Engineering in China, vol. 2, no. 4, pp. 457-460.
 
[9]  H. Tamaki (2013), Study on flow fields in high specific speed centrifugal compressor with unpinched vaneless diffuser, Journal of Mechanical Science and Technology, vol. 27, no. 6, pp. 1627-1633.
 
[10]  M. Kalinkevych and O. Shcherbakov (2013), Numerical Modeling of the Flow in a Vaneless Diffuser of Centrifugal Compressor Stage, ISRN Mechanical Engineering, 2013.
 
[11]  A. N. Abdelhamid (1983), Effects of Vaneless Diffuser Geometry on Flow Instability in Centrifugal Compression Systems, Canadian Aeronautics and Space Journal, vol. 29, no. 2, pp. 259-266.
 
[12]  Y. Kinoshita and Y. Senoo (1985), Rotating Stall Induced in Vaneless Diffusers of Very Low Specific Speed Centrifugal Blowers, Journal of Engineering for Gas Turbines and Power, vol. 107, no. 2, pp. 514-521, 1985.
 
[13]  A. Jaatinen-Varri, P. Roytta, T. Turunen-Saaresti, and A. Gronman (2013), Experimental Study of Centrifugal Compressor Vaneless Diffuser Width, Journal of Mechanical Science and Technology, vol. 27, no. 4, pp. 1011-1020.
 
[14]  R. Aungier (1988), A Systematic Procedure for the Aerodynamic Design of Vaned Diffusers. ASME FED, 69, 27-34.
 
[15]  Y. Yoshinaga, I. Gyobu, H. Mishina, F. Koseki and H. Nishida (1980), Aerodynamic Performance of a Centrifugal Compressor WithVaned Diffusers, Transaction of ASME, vol. 102, 486-493.
 
[16]  C. Rodgers. (1982), The performance of centrifugal compressor channel diffusers, New York, ASME-82-GT-10.
 
[17]  U.Haupt, U. Seidel, A. N. Abdul-Hamid and M. Rautenberg (1988), Unsteady Flow in a Centrifugal Compressor with Different Types of Vaned Diffusers, New York: American Society of Mechanical Engineers, ASME/88-GT-22.
 
[18]  Kim, W. and Engeda, A. (1997), Comparison of Pressure Recovery and Overall Performance of Different Diffusers for Centrifugal Compressor, In FEDSM97-3029 Fluids Engineering Division Summer Meeting, ASME.
 
[19]  F. Justen, K. U. Ziegler and H. E. Gallus (1999), Experimental investigation of unsteady flow phenomena in a centrifugal compressor vaned diffuser of variable geometry, New York, ASME, ASME/98-GT-368.
 
[20]  N. He and A. Tourlidakis, (2001), Analysis of Diffusers with Different Number of Vanes in a Centrifugal Compressor Stage, In 2001-GT-0321, ASME TURBO EXPO.
 
[21]  Kim, Y., Engeda, A., Aungier, R., &Amineni, N. (2002), A centrifugal compressor stage with wide flow range vaned diffusers and different inlet configurations, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 216(4), 307-320.
 
[22]  A. Engeda (2003), Experimental and Numerical Investigation of the Performance of a 240 kW Centrifugal Compressor with Different Diffusers, Experimental Thermal and Fluid Science, 28(1), 55-72.
 
[23]  T. Turunen-Saaresti (2004), Computational and Experimental Analysis of Flow Field in the Diffusers of Centrifugal Compressors, PhD thesis, Lappeenranta University of Technology.
 
[24]  J. Issac, N. Sitaram, and M. Govardhan (2004), Effect of Diffuser Vane Height and Position on the Performance of a Centrifugal Compressor, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 218(8):647-654.
 
[25]  M. Kalinkevych, O. Obukhov, A. Smirnov, and A. Skoryk (2011), The design of vaned diffusers of centrifugal compressors based on the given velocity distribution, in Proceedings of the 7th International Journal of Rotating Machinery 7 International Conference on Compressors and their Systems, pp. 61-69, Woodhead Publishing, 2011.
 
[26]  M. Kalinkevych and A. Skoryk (2013), Design Method for Channel Diffusers of Centrifugal Compressors, International Journal of Rotating Machinery.
 
[27]  T. C. S. Reddy, G. R. Murty and MVSSSM. Prasad (2014), Effect of diffuser vane shape on the performance of a centrifugal compressor stage, Journal of Thermal Science, 23(2), 127-132.
 
[28]  C. Osborne, and J. Sorokes (1988), The Application of Low Solidity Diffusers in Centrifugal Compressors, Flows in Non-Rotating Turbomachinery Components, ASME FED-Vol 69, pp. 89-101.
 
[29]  J. M. Sorokes and J. P. Welch (1991), Centrifugal Compressor Performance Enhancement Through the Use of Single-Stage Development Rig, In Proceedings of the 20th Turbomachinery Symposium, Texas A&M (pp. 101-112).
 
[30]  .M. Sorokes, and J.P. Welch (1992), Experimental Results on a Rotatable Low Solidity Vaned Diffuser, ASME Preprint 92-GT-19.
 
[31]  Y. Galerkin, K. Soldatova and O. Solovieva, (2015), Numerical Study of Centrifugal Compressor Stage Vaneless Diffusers, In IOP Conference Series: Materials Science and Engineering (Vol. 90, No. 1, p. 012048), IOP Publishing.
 
[32]  Cheng Xu and Ryoichi. S. Amano (2012), Empirical design considerations for industrial centrifugal compressors, International Journal of Rotating Machinery, vol. 2012 (2012), Article ID: 18406.
 
[33]  C. Rodgers (1978), A Diffusion Factor Correlation for Centrifugal Impeller Stalling, 78-GT-61.
 
[34]  W. Jansen (1967), A method for Calculating the Flow in a Centrifugal Impeller When Entropy Gradients are Present, Institution of Mechanical Engineers, Royal Society Conference on Internal Aerodynamics (Turbomachinery ) , pages: 133-146.
 
[35]  Barend W. Botha and AdriaanMoolman (2005), Determining the Impact of the Different Losses on Centrifugal Compressor Design, R & D Journal, 2005, 21 (3) incorporated into The SA Mechanical Engineer.
 
[36]  O.F. Okhuahesogie, J. Stewart, F.J.G. Heyes and P.E. Roach (2012), Design Optimization of Two-Stage Turbocharger Compressor Impeller, KTP Associates Conference, University of Brighton, UK, 14 June 2012.
 
[37]  R. Aungier (1997), Design of Centrifugal Compressor Stage for Enhanced Operating Range and Head Rise, Internal Report (Cited in Kim et al., 2002).
 
[38]  Stanitz JD (1952), Some Theoretical Aerodynamic Investigations of Impellers in Radial and Mixed-Flow Centrifugal Compressors, Cleveland, Ohio, Transactions of the ASME, Vol. 74, 473-476.
 
[39]  Hohlweg, W. C., Direnzi, G. L., &Aungier, R. H. (1993, May), Comparison of Conventional and Low Solidity Vaned Diffusers, In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition (pp. V001T03A039-V001T03A039). American Society of Mechanical Engineers.