Experimentally Investigation on Combustion Phenomena in Micro Combustor for the Application of Power MEMS

초소형 연소기에서의 연소 현상 실험적 연구

  • 나한비 (한국항공우주연구원 추진제어그룹) ;
  • 김세훈 (KAIST 항공우주공학전공 대학원) ;
  • 최원영 (KAIST 항공우주공학전공 대학원) ;
  • 권세진 (KAIST 항공우주공학전공)
  • Published : 2003.05.01

Abstract

The characteristic of constant volume micro combustor was investigated experimentally. The shape of micro combustor was cylindrical and has row aspect ratio or has relatively large diameter compared with chamber height. Diameter and chamber height was varied to investigate the geometric effect of combustor on the flame propagation. Diameter of 15 mm and 7.5 mm was designed while chamber height was designed to be 1mm, 2mm, and 3mm. The effect of initial pressure was also investigated parametrically from 1bar to 3bar. The gas used in this study was stoichiometric mixture of methane and air. The maximum pressure achieved in down scaled combustors was lower than that of conventional combustor because heat loss to wall was dominant as expected. The maximum pressure responded favorably with the change of height of combustor and the initial pressure, the maximum pressure was also increased. The flame propagation was possible when the specific condition was satisfied. Although the quenching distance of stoichiometric mixture of CH4 and Air is 2.5 mm, the flame could propagate even under quenching distance as the initial pressure increased.

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