Design of a Centrifugal Compressor with Low Solidity Vaned Diffuser (LSVD) for Large-Scale Compressed Air Energy Storage (CAES)

Compressed Air Energy Storage (CAES) has tremendous promotional value in the intermittent renewable energy supply systems. CAES has special requirements for compressor (e.g. heavy load, high pressure ratio, wide range). With advantages of higher efficiency and wider operation range, IGC (Integrally Geared Compressors) is selected to fulfill the special requirements of the large-scale CAES. To get a better aerodynamic performance, in this paper, based on the analysis of internal flow of centrifugal compressor, a multi-objective one-dimensional optimization design program was put forward combined with modified Two-Zone model and a low solidity vaned diffuser (LSVD) design method. Then, a centrifugal compressor aerodynamic component optimization design system was established with the three-dimensional blade optimization design method based on neural network and genetic optimization algorithm. Then a validation was done by redesigning the Krain-Impeller to get better performance. Finally, the aerodynamic design of the first stage of IGC was completed. The CFD calculation results indicated that the total-to-total pressure ratio of the first stage was 2.51 and the polytropic efficiency was 91.0% at the design point. What’s more, an operation margin and surge margin of the compressor was about 26.5% and 16.4% respectively.

[1]  R. Dean,et al.  Rotating Wakes in Vaneless Diffusers , 1960 .

[2]  D. Japikse,et al.  Assessment of Single- and Two-Zone Modeling of Centrifugal Compressors, Studies in Component Performance: Part 3 , 1985 .

[3]  Abraham Engeda,et al.  Design and optimization of a single stage centrifugal compressor for a solar dish-Brayton system , 2013 .

[4]  Andrea Arnone,et al.  Development of Secondary Flow Field in a Low Solidity Diffuser in a Transonic Centrifugal Compressor Stage , 2002 .

[5]  C. J. Robinson,et al.  Centrifugal compressor design , 1998 .

[6]  Haisheng Chen,et al.  Progress in electrical energy storage system: A critical review , 2009 .

[7]  Toshiharu Kazama,et al.  On the effects of the temperature profile approximation in thermal Newtonian solutions of elastohydrodynamic lubrication line contacts , 2001 .

[8]  Pericles Pilidis,et al.  A new method for reliable performance prediction of multi-stage industrial centrifugal compressors based on stage stacking technique: Part I – existing models evaluation , 2016 .

[9]  Hartmut Krain Review of Centrifugal Compressor’s Application and Development , 2005 .

[10]  H. Hayami,et al.  Application of Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor , 1989 .

[11]  Naresh K. Amineni,et al.  A centrifugal compressor stage with wide flow range vaned diffusers and different inlet configurations , 2002 .

[12]  H. W. Oh,et al.  Systematic two-zone modelling for performance prediction of centrifugal compressors , 2002 .

[13]  J. E. Donald Gauthier,et al.  Performance Prediction of Centrifugal Impellers Using a Two-Zone Model , 2008 .

[14]  H. Krain,et al.  Verification of an Impeller Design by Laser Measurements and 3D-Viscous Flow Calculations , 1989 .

[15]  Beat Ribi,et al.  Radial compressor design for industrial compressors , 1999 .

[16]  D. Japikse Centrifugal compressor design and performance , 1996 .

[17]  Michael D. Hathaway,et al.  Laser Anemometer Measurements of the Three-Dimensional Rotor Flow Field in the NASA Low-Speed Centrifugal Compressor , 1995 .

[18]  D. Eckardt,et al.  Instantaneous Measurements in the Jet-Wake Discharge Flow of a Centrifugal Compressor Impeller , 1975 .

[19]  A Engeda The design and performance results of simple flat plate low solidity vaned diffusers , 2001 .

[20]  William C. Hohlweg,et al.  Comparison of Conventional and Low Solidity Vaned Diffusers , 1993 .

[21]  R. E. Nece,et al.  Chamber Dimension Effects on Induced Flow and Frictional Resistance of Enclosed Rotating Disks , 1960 .