A study on the performance characteristics of annular-reverse combustor for APU

환형역류형 APU 연소기 성능특성 연구

  • 이동훈 (삼성테크원 파워시스템 연구소) ;
  • 최성만 (삼성테크원 파워시스템 연구소) ;
  • 한영민 (한국항공우주연구원 추진성능시험그룹) ;
  • 고영성 (한국항공우주연구원 추진성능시험그룹)
  • Published : 2001.06.01

Abstract

The annular-reverse combustor was designed for APU combustor and a three dimensional analysis for reactive flow in the combustor was performed. At the same time, the experimental work was performed in KARl combustor test facility. In this study we found out that tangential swirl type combustor is good for flame holding than single vortex type combustor. The flame tube main hole size and relative position are very important parameters for combustor general performance. The ignition characteristics are strongly depend on the air fuel ratio with combustor inlet volume flow ratio.

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