Development of High Efficiency Gas Turbine/Fuel Cell Hybrid Power Generation System

가스터빈/연료전지 혼합형 고효율 발전시스템 개발

  • 김재환 (항공사업기획그룹, 한국항공우주연구원) ;
  • 박부민 (항공추진그룹, 한국항공우주연구원) ;
  • 양수석 (항공추진그룹, 한국항공우주연구원) ;
  • 이대성 (항공사업단, 한국항공우주연구원)
  • Published : 2005.06.01

Abstract

This paper describes an on-going national R&D program for the development of a gas turbine/fuel cell hybrid power generation system and related R&D activities. The final goal of this program is to develop a 200kW-c1ass gas turbine/fuel cell hybrid power generation system and achieve high efficiency over $60\%$ (AC/LHV). In the first phase of the development, a sub-scaled 60kW-class hybrid system based on the 50kW-class microturbine and the 5kW SOFC will be developed for the purpose of concept proof of the hybrid system. Core components such as the microturbine and the SOFC system are being developed and parallel preparation for system integration is being carried out. Before the core components are assembled in the final system. operating characteristics of a hybrid system are investigated from a simulated system where a turbocharger (microturbine simulator) and a modified fuel cell burner test facility (fuel cell simulator) are employed. The 60kW demonstration unit will be built up and operated to provide the valuable information for the preparation of the final full scale 200kW hybrid system.

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