Study on Numerical Analysis for Ram-Air flow of Cooling Duct on the Propulsion System

추진시스템 냉각유로의 주행풍 유동에 대한 수치해석적 연구

  • 유성열 (성균관대학교 대학원, 기계공학부) ;
  • 조정래 (성균관대학교 대학원, 기계공학부) ;
  • 조태식 (성균관대학교 대학원, 기계공학부) ;
  • 김철주 (성균관대학교, 기계공학부)
  • Published : 2009.05.21

Abstract

The cooling technology of power conversion semiconductors in the propulsion system for the HEMU(High Electrical Multi Unit) are applied in water cooling method and phase change method such as the immersed type and the heat pipe type. Both of cooling systems need a condenser and a fan through forced wind to emit that is radiated heat from electric power conversion semiconductor(IGBT) stack effectively, now in the case of Japanese Fastec 360S, is using ram-air that is flowed in establishing cooling passage to propulsion system for cooling of condenser. In this research, it is that achieved the computing numerical analysis using ADINA of commertial program to examine flow characteristics and pressure distribution of ram-air for a condenser in cooling passage.

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