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LIU Xiaodong(刘晓东), FU Bao(付豹), ZHUANG Ming(庄明). The Design and Analysis of Helium Turbine Expander Impeller with a Given All-Over-Controlled Vortex Distribution[J]. Plasma Science and Technology, 2014, 16(3): 288-293. DOI: 10.1088/1009-0630/16/3/21
Citation: LIU Xiaodong(刘晓东), FU Bao(付豹), ZHUANG Ming(庄明). The Design and Analysis of Helium Turbine Expander Impeller with a Given All-Over-Controlled Vortex Distribution[J]. Plasma Science and Technology, 2014, 16(3): 288-293. DOI: 10.1088/1009-0630/16/3/21

The Design and Analysis of Helium Turbine Expander Impeller with a Given All-Over-Controlled Vortex Distribution

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  • Received Date: July 18, 2012
  • To make the large-scale helium cryogenic system of fusion device EAST (experimen- tal advanced super-conducting tokamak) run stably, as the core part, the helium turbine expander must meet the requirement of refrigeration capacity. However, previous designs were based on one dimension flow to determine the average fluid parameters and geometric parameters of impeller cross-sections, so that it could not describe real physical processes in the internal flow of the tur- bine expander. Therefore, based on the inverse proposition of streamline curvature method in the context of quasi-three-dimensional flows, the all-over-controlled vortex concept was adopted to design the impeller under specified condition. The wrap angle of the impeller blade and the whole flow distribution on the meridian plane were obtained; meanwhile the performance of the designed impeller was analyzed. Thus a new design method is proposed here for the inverse proposition of the helium turbine expander impeller.
  • 1 Bai Hongyu. 2002, Thermodynamic Analysis and de-sign of the helium refrigeration system for HT-7U su-perconducting tokamak [Ph.D]. Institute of plasma physics, Chinese Academy of Sciences, Hefei (in Chi-nese) ;
    2 Bai Hongyu, Bi Yanfang, Zhu Ping, et al. 2006, Fusion Engineering and Design, 81: 2597;
    3 Bai Hongyu, Bi Yanfang, Wang Jinrong, et al. 2002,Fusion Science and Technology, 42: 162;
    4 Ji Guanghua. 1989, Turbo-expander. China machine Press, Beijing (in Chinese) ;
    5 Wang Shangjin. 1991, Three-dimensional flow theory and application to Centrifugal compressor. Xi'an jiao-tong Univ. Press, Xi'an (in Chinese) ;
    6 Wu Chung-Hua. 1952, A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbo-machines of Axial-, Radial-, and Mixed-Flow Types.NACA TN 2604;
    7 Borges J E. 1990, A three-dimensional inverse method for turbomachinery: Part 1-Theory. ASME J Turbo-machinery, 11: 346;
    8 Katsanis, Theodore. 1964, Use of Arbitrary Quasi-Orthogonals for Calculating Flow Distribution In the Meridional Plane Of A Turbomachine. NASA TN D-2546 ;
    9 Michael R Vanco. 1972, FORTRAN Program for Cal-culating Velocities in the Meridional Plane of a Tur-bomachine Ⅰ- Centrifugal Compressor, NASA TN D-7601;
    10 John D Stanitz and Vasily D Prian. 1951, A Rapid Approximate Method for Determining Velocity Distri-bution on Impeller Blades of Centrifugal Compressors.NACA TN2421;
    11 Zangeneh M, Goto A, and Takemura T. 1996, Sup-pression of secondary flows in a mixed-flow pump impeller by application of three-dimensional inverse design method. 1: Design and numerical validation. Transactions of ASME, 118: 536-551;
    12 Zangeneh M. 1991, International Journal of Numerical Methods in Fluids, 13: 599 ;
    13 Li Chao, Zhang Ruicheng. 2003, Journal of Power En-gineer, 23: 2845 (in Chinese)

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