충돌제트 버너에서 합성가스( H₂/CO )/공기 예혼합화염의 안정화 특성
Stability Characteristics of Syngas(H₂/CO )/Air Premixed Flames using an Impinging Jet Burner
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초록
An experimental study was conducted to investigate the flame stability of the synthetic gas (syngas) using an impinging premixed jet burner. Since the syngas mainly consisted of H2 and CO, the H₂/CO mixture was simulated as the syngas. H₂/CO mixture ratios, fuel/air mixture velocities and equivalence ratios were used as major parameters on the flame stability. The role of the impinging plate on the flame stability was also examined. In addition, laminar burning velocities of the H₂/CO mixture were predicted numerically to understand the characteristics of the flame stability for the syngas. The increase in the H2 concentration into the syngas brings about the extension of the blowout limit and the reduction in the flashback limit in terms of the stable flame region. The impinging jet plate broadened the blowout limit but does not play important role in changing of the flashback limit. Finally, it was found that the stability region of the flame using the syngas, which is expressed in terms of the mixture velocity and the equivalence ratio in this study, significantly differed from that of CH4.
Abstract
An experimental study was conducted to investigate the flame stability of the synthetic gas (syngas) using an impinging premixed jet burner. Since the syngas mainly consisted of H2 and CO, the H₂/CO mixture was simulated as the syngas. H₂/CO mixture ratios, fuel/air mixture velocities and equivalence ratios were used as major parameters on the flame stability. The role of the impinging plate on the flame stability was also examined. In addition, laminar burning velocities of the H₂/CO mixture were predicted numerically to understand the characteristics of the flame stability for the syngas. The increase in the H2 concentration into the syngas brings about the extension of the blowout limit and the reduction in the flashback limit in terms of the stable flame region. The impinging jet plate broadened the blowout limit but does not play important role in changing of the flashback limit. Finally, it was found that the stability region of the flame using the syngas, which is expressed in terms of the mixture velocity and the equivalence ratio in this study, significantly differed from that of CH4.
참고문헌 (13)
- Z. Zhang, "Measurements of laminar burning velocities and Markstein lengths for methanol", air, Combustion and Flame, pp.2008, 155[DOI]
- C. Prathap, "Investigation of nitrogen dilution effects on the laminar burning velocity and flame stability of syngas fuel at atmospheric condition", Combustion and Flame, 155, pp.145~160 (2008)
- 김태권, "H₂", CO 합성가스의 연소 특성에 관한 연구, 2008, pp.17(6), 689~698[DOI]
- J. Natarajan, "Laminar flame speeds of H2", CO mixtures: Effect of CO2 dilution, preheat temperature, and pressure, 2007, pp.151, 104~119
- 최상규, "합성가스의 연소특성에 대한 수치적 연구", 한국자동차 공학회 춘계학술대회논문집, pp.626~632 (2006), 한국자동차 공학회
- S. G. Tuttle, "Convective heat transfer from a partially premixed impinging flame jet. Part I: Time- averaged results", International Journal of Heat and Mass Transfer, 48, pp.1236~1252 (2005)
- Subhash Chander, "Flame impingement hear transfer : A review", Energy Convertsion and Management, 46, pp.2803~2837 (2005)
- W. -D. Hsieh, "Methane flame stability in a jet impinging onto a wall", Energy Conversion and Management, 46, pp.727~739 (2005)
- A frotran program for modeling steady laminar one-dimensional premixed flame, "R. J. Kee", ~, pp.Sandia Report 85-8240
- S. G. Davis, "An optimized kinetic model of H2", CO combustion, 2005, pp.30, 1283~1292
- Chemkin-II: A frotran chemical kinetics package for the analysis of gas phase chemical kinetics, "R. J. Kee", ~, pp.Sandia Report 89-8009B (1989)
- A fortran computer code package for the evaluation of gas-phase multi-component transport properties, "R. J. Kee", ~, pp.Sandia Report SAND86-8246 (1994)
- Nicolas Bouvet, "Experimental studies of the fundamental flame speeds of syngas(H2", CO), Proceedings of the Combustion Institute, pp.2010[DOI]
