• 한국연소학회:학술대회논문집
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• 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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• pp.81-84
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• 2014

A Experimental study on flame extinction behavior was investigated using He curtain flow with counter triple co-flow burner. Buoyancy force was suppressed up to a microgravity level of $10^{-2}-10^{-3}g$ by using He curtain flow. The stability maps were provided with a functional dependency of diluent mole fraction and global strain rate to clarify the differences in flame extinction behavior. The flame extinction curves had C-shapes at various global strain rates. The oscillation and extinction modes were different each other in terms of the global strain rate, and the flames extinction modes could be classified into five modes such as (I) and (II): an extinction through the shrinkage of the outmost edge flame forward the flame center after self-excitation and without self-excitation, respectively, (III): an extinction through rapid advancement of a flame hole while the outmost edge flame is stationary, (IV): self-excitation occurs in the outermost edge flame and the center edge flame and then a donut shaped flame is formed and/or the flame is entirely extinguished, (V): shrinkage of the outermost edge flame without self-excitation followed by shrinkage or survival of the center flame. These oscillation and extinction modes could be identified well to the behavior of edge flame. The result also showed that the edge flame was influenced significantly by the conductive heat losses to the flame center or ambient He curtain flow.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2000년도 제21회 KOSCO SYMPOSIUM 논문집
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• pp.77-82
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• 2000

Numerical simulations of freely propagating flames burning stoichiometric $CH_4$/$O_2$/$N_2$ mixtures are performed at atmospheric pressure in order to understand the effect of the $O_2$ enrichment level on $CH_4$/Air flame. A chemical kinetic mechanism is employed, the adopted scheme involving 54 gas-phase species and 632 forward reactions. The calculated flame. speeds are compared with the experiments for the flames established at several $O_2$ enrichment level, the results of which is in excellent agreement. As a result of the increased $O_2$ enrichment level from 0.21 to 1, the mole fraction of CO in the burned gas is increased. The flame speed and the temperature in the burned gas are also increased, but the thickness of the flame is severely shrunken in the preheat region.

• 한국연소학회지
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• 제7권4호
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• pp.36-44
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• 2002

Carbon molecules with closed-cage structures are called fullerenes $(C_{60},\;C_{70})$, whose applications include super-conductors, sensors, catalysts, optical and electronic device, polymer composites, and biological and medical materials. The synthesis of fullerenes has been recently studied with low-pressure benzene/argon/oxygen flames. The formation of fullerene is known as molecular weight growth processes of PAHs (polycyclic aromatic hydrocarbon). This study presents results of PAHs and fullerene measurements performed in a low-pressure benzene/argon/oxygen normal co-flow laminar diffusion flame. Through the central tube of the burner, benzene vapors carried by argon are injected. The benzene vapors are made in a temperature-controlled bubbler. The burner is located in a chamber, equipped with a sampling system for direct collection of condensable species from the flame, and exhausted to a vacuum pump. Samples of the condensable are analyzed by HPLC (High Performance Liquid Chromatography) to determine the yields of PAHs and fullerene. Also, we computed mole fraction of fullerene and PAHs in a nearly sooting low pressure premixed, one-dimensional benzene/argon/oxygen flame (equivalence ratio ${\Phi}=2.4$, pressure=5.33kPa). The object of computation was to investigate the formation mechanism of fullerenes and PAHs. The computations were performed with CHEMKIN/PREMIX. As a result of this study, fullerenes were synthesized in a low pressure (20torr) $C_6H_6/Ar/O_2$ flames and the highest concentration of fullerene was detected just above the visible surface of a flame.

• 한국가스학회지
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• 제26권3호
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• pp.45-53
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• 2022

디젤엔진의 배출물 개선을 위해 탄소수가 낮은 천연가스를 혼합하여 사용하는 천연가스-디젤 혼소 연소가 각광받고 있다. 특히 자발화 특성에 차이가 있는 디젤과 천연가스의 특성을 이용한 반응성 제어 압축착화(reactivity controlled compression ignition, RCCI) 연소 전략을 통해 기존 디젤엔진의 효율과 배출가스를 동시에 개선시키는 연구가 활발하게 진행되어 왔다. 상사점보다 앞당겨진 디젤 직접 분사시기 적용을 통해 실린더 전체 영역의 균일 혼합기를 형성하여 전체적으로 희박한 자발화 기반 연소를 달성함으로써 질소산화물 (NOx) 및 입자상물질 (PM) 저감과 제동열효율 개선을 동시에 달성할 수 있다. 하지만 매우 희박한 저부하 영역에서 불완전 연소량이 증가하는 단점이 존재하며, 안정적인 연소 구현을 위해 디젤 분사시기가 민감하게 제어되어야 하는 어려움도 존재한다. 본 연구에서는 앞서 언급된 저부하 영역에서의 천연가스-디젤 혼소 엔진의 효율 및 배기 개선을 확인하고, 동시에 발전용 엔진 구동 영역에서 디젤 분사시기에 따른 연소안정성을 평가하였다. 실험에는 6 L급 상용디젤 엔진이 사용되었으며, 1,800 rpm, 50% 부하 영역 (~50 kW)에서 실험이 진행되었다. 제동효율 및 연소안정성을 개선하기 위한 전략으로 분무 패턴이 다른 2개의 인젝터를 적용하였으며, 천연가스/디젤 비율과 디젤 분사시기를 바꿔가면서 실험이 진행되었다. 실험 결과, 협각 분사가 추가된 수정 인젝터에서 제동 열효율이 증가하는 것을 확인하였다. 또한 연소안정성 및 출력, 그리고 강화된 배기 규제를 고려하였을 때 수정 인젝터의 분무 패턴이 예혼합연소 형성에 적합하였고 이를 통해 질소산화물 배출량을 Tier-V 기준치인 0.4 g/kWh 이하로 저감함으로써 RCCI 연소 가능 영역을 확장할 수 있음을 실험적으로 확인하였다.