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원심압축기의 링 그루브 효과에 관한 수치해석적 연구

Numerical Investigation of Ring Groove Effect in a Centrifugal Compressor

  • 박치용 (한양대학교 대학원 한국생산기술연구원) ;
  • 최영석 (한국생산기술연구원 에너지설비센터) ;
  • 이경용 (한국생산기술연구원 에너지설비센터) ;
  • 윤준용 (한양대학교 기계공학과)
  • 투고 : 2010.05.31
  • 심사 : 2011.02.10
  • 발행 : 2011.04.01

초록

This paper presents a numerical study of casing treatments on a centrifugal compressor stage to improve stability and the surge margin. High efficiency, a high pressure ratio, and a wide operating range are required for a high performance centrifugal compressor. In the present study, a ring groove arrangement was applied to the transonic centrifugal compressor. According to the numerical analysis using a commercial code ANSYS-CFX, the unstable phenomena limiting the range of the centrifugal compressors were compared with and without a ring groove. Although the ring groove decreased the efficiency, but increased the operating range by suppressing a flow separation at the leading-edge of the impeller especially near shroud part. Newly designed ring groove arrangement improved the compressor performance and increased the operating range of the compressor.

키워드

참고문헌

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