Flow Structure Interaction 3-D Reciprocating Compressor and Impact Analyses of Compressor Discharge Valve

압축기 토출벨브의 유체-구조 연계해석 및 충돌해석

  • 레사 옥타비안티 (국립경상대학교 기계항공공학부 대학원) ;
  • 김동현 (국립경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 박강균 (국립경상대학교 기계항공공학부 대학원) ;
  • 정원현 (국립경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 안재우 (국립경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 문경호 (국립경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 고영필 (국립경상대학교 기계항공공학부 및 항공기부품기술연구소) ;
  • 김형식 (LG 전자(주) DAC 연구소)
  • Published : 2007.05.10

Abstract

In this paper, 3-D reciprocating compressor is taken into flow-structure interaction analysis. The full cycle process consisted of cylinder expansion and compression has been modeled without considering flow leakage through cylinder wall. Fully-coupled FSI analysis of this compressor model was iteratively solved and gives sufficient result with the experimental test. The study is emphasized to thoroughly investigate discharge valve motion, opening and closing, in order to determine discharge valve region which is prone to have high effective stress. The cylinder pressure is successfully validated before conducting impact analyses between discharge valve and other susceptible supported structure. Velocity profile has been obtained in FSI analysis is used as initial condition to carry out further impact analyses. Stress result of discharge valve and valve spring gives preliminary estimation of higher stress area due to its impact phenomena.

Keywords