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SOFC-GT 혼합시스템용 원심압축기 공력설계 및 유동특성 연구

A Study on Aerodynamic Design and Flow Characteristics of a CentrifugalCompressor for SOFC-Gas Turbine Hybrid System

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초록

This study presents an aerodynamic design and numerical analysis of a centrifugal compressor in gas turbines for SOFC-gas turbine hybrid system application. Total-to-total pressure ratio of the compressor is 3.6:1 that could be used widely for small and large SOFC-gas turbine systems. The compressor consists of a centrifugal impeller and a wedge diffuser. Conceptual design and aerodynamic design with mean line analysis and quasi-3D analysis are performed, and aerodynamic parameters as well as design variables are discussed from the design results. A numerical analysis based on the Reynolds-averaged Navier-Stokes equation was performed for the flow analysis of the compressor. The results show that the centrifugal compressor designed meets the design target, and the aerodynamic parameters and results of the compressor can be used for the aerodynamic design of centrifugal compressors and the feasibility study of SOFC-gas turbine system design.

Abstract

This study presents an aerodynamic design and numerical analysis of a centrifugal compressor in gas turbines for SOFC-gas turbine hybrid system application. Total-to-total pressure ratio of the compressor is 3.6:1 that could be used widely for small and large SOFC-gas turbine systems. The compressor consists of a centrifugal impeller and a wedge diffuser. Conceptual design and aerodynamic design with mean line analysis and quasi-3D analysis are performed, and aerodynamic parameters as well as design variables are discussed from the design results. A numerical analysis based on the Reynolds-averaged Navier-Stokes equation was performed for the flow analysis of the compressor. The results show that the centrifugal compressor designed meets the design target, and the aerodynamic parameters and results of the compressor can be used for the aerodynamic design of centrifugal compressors and the feasibility study of SOFC-gas turbine system design.

참고문헌 (12)

  1. Turbo-Machinery Requirements for Practical SOFC-Gas Turbine Hybrid Systems, "R.W.Schonewal", ~, pp.ASME Paper No. GT2005-69127 (2005)
  2. Design and Off-Design Analysis of a MW Hybrid System Based on Rolls-Royce Integrated Planar SOFC, "L. Magistri", ~, pp.ASME Paper No. GT2003-38220 (2003)
  3. The Design and Integration of the Rolls-Royce Fuel Cell Systems 1MW SOFC, "Agnew, G. D.", ~, pp.ASME Paper No. GT2005-69122 (2005)
  4. Comparative Evaluation of SOFC, "Gas Turbine Hybrid System Options", K. P. Litzinger, 2005, ASME Paper No. GT2005- 68909
  5. Sensitivity Analysis of Transient Compressor Operation Behaviour in SOFC-GT Hybrid Systems, "A. Hildebrandt", ~, pp.ASME Paper No. GT2005-68744 (2005)
  6. 송락현, "원통형 고체산화물 연료전지 기술개발", 2001 유체기계 연구개발 발표회, pp.373~380 (2001)
  7. 김명환, "선박 동력발생용 연료전지시스템 기술개발의 전망에 대한 고찰", 한국마린엔지니어링학회지, 31(8), pp.924~931 (2007), 한국마린엔지니어링학회
  8. Numerical and Experimental Investigation on a High Pressure Ratio Centrifugal Compressor, "J. H. Choi", ~, pp.Paper No. GT2005-68679 (2005)
  9. D. Japikse, "Centrifugal Compressor Design and Performance" (1996), Concepts ETI
  10. "COMPAL Version 7.9.30, Concepts NREC", ~ (2006)
  11. "AXCENT Version 7.9.18.40, Concepts NREC", ~ (2007)
  12. "CFX-TASCFlow, ANSYS", ~ (2005)

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