• 한국연소학회지
• /
• 제11권2호
• /
• pp.22-27
• /
• 2006

This experimental study has been mainly motivated to obtain generally applicable design correlation for the front mixing premix combustor. The design concept of the front mixing premix combustor is to minimize thermal $NO_x$ and prompt $NO_x$ formation by maintaining low peak flame temperature, and nearly uniform flame temperature through rapid mixing process near the ignition point. The present experimental results clearly indicate that the front mixing premix combustor yields the $NO_x$ level lower than 43 ppm $NO_x$ emissions and the nearly uniform temperature distribution.

• 한국자동차공학회논문집
• /
• 제11권5호
• /
• pp.60-69
• /
• 2003

The simplified two-color method is proposed which can estimate the temperature distribution and the soot density of the whole flame with the image analysis of the high-speed photographs. The factors influenced on its processing were examined, for example, the selection of the wave length, the kind of films, the preparation of the calibration curve between the radiance of flame and the luminance temperature. The simplified two-color method reported in this paper can be used as a tool for the improvement of the combustion process in direct injection diesel engine.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2013년도 제46회 KOSCO SYMPOSIUM 초록집
• /
• pp.107-108
• /
• 2013

An experimental study in the dual swirl burner was conducted to analyze the temperature characteristics in the combustion field. The dual swirl burner consists of a main swirling pre-mixed flame with tangential swirler surrounding a pilot which can stabilize a diffusion flame or a partially premixed flame with vane swirler depending on whether fuel is supplied at the exit plane or further upstream. The purpose of this study is to analyse experimentally the characterization of flame temperature in the reacting zone, specially, according to the various combustor diameters like 80mm, 100mm, 130mm and 150mm(O.D). As a result, the temperatures of combustion field were decreased as the diameter of combustor increased. Therefore, these results can be expected that the larger diameter of combustor tend to emit less NOx emission than the small combustor.

• 대한기계학회논문집B
• /
• 제28권3호
• /
• pp.359-364
• /
• 2004

For the development of high efficiency and low emission combustion systems, high temperature air combustion technology has been tested by utilizing preheated air over 1100 K and exhaust gas recirculation. In this system, combustion air is diluted with large amount of recirculated exhaust gases, such that the oxygen concentration is relatively low in the reaction zone, leading to low flame temperature. Since, the temperature fluctuations and sound emissions from the flame are small and flame luminosity is low, the combustion mode is expected to be flameless or mild combustion. Experiment was performed to investigate the turbulent flame structure and NO$_x$ emission characteristics in the high temperature air combustion focused on coflowing jet diffusion flames which has a fundamental structure of many practical combustion systems. The effect of turbulence has also been evaluated by installing perforated plate in the oxidizer inlet nozzle. LPG was used as a fuel. Results showed that even though NO$_x$ emission is sensitive to the combustion air temperature, the present high temperature air combustion system produce low NO$_x$ emission because it is operated in low oxygen concentration condition by the high exhaust gas recirculation.

• 한국연소학회:학술대회논문집
• /
• 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
• /
• pp.89-94
• /
• 2003

For the development of high efficiency and low emission combustion systems, high temperature air combustion technology has been tested by utilizing preheated air over 1100 K and exhaust gas recirculation. In this system, combustion air is diluted with large amount of exhaust gases ($N_2$, $CO_2$), such that the oxygen concentration is relatively low in the reaction zone, leading to low flame temperature. Since, the temperature fluctuations and sound emissions form the flame are small and flame luminosity is low, the combustion mode is expected to be flameless or mild combustion. Experiment was performed to investigate the turbulent flame structure and $NO_X$ emission characteristics in the high temperature air combustion focused on coflowing jet diffusion flames which has a fundamental structure of many practical combustion systems. The effect of turbulence has also been evaluated by installing perforated plate in the oxidizer inlet nozzle. LPG was used as a fuel. Results showed that even though $NO_X$ emission is sensitive to the combustion air temperature, the present high temperature air combustion system produce low $NO_X$ emission because it is operated in low oxygen concentration condition in excess of dilution.

• 한국화재소방학회논문지
• /
• 제24권6호
• /
• pp.170-175
• /
• 2010

동축류버너를 이용한 제트확산화염에서 이산화탄소의 첨가가 매연 생성에 미치는 영향을 조사하였다. R-타입 열전대를 이용하여 화염대 및 황염과 청염의 경계온도를 측정하였다. 광감쇄법을 이용하여 화염이 존재하는 국소부분에서의 상대적인 매연 농도(1-I/$I_0$)를 측정하였다. 광원으로는 파장이 632.8nm인 He-Ne 레이저가 사용되었고 디텍터를 이용하여 매연입자에 의해 산란과 흡수를 겪은 후의 감쇄된 신호를 직접 측정하였다. 또한, 매연 생성에 있어서의 열적 효과를 알아보기 위해 산화제의 유속을 변화시켜 유속에 의한 영항을 알아보았다. 실험 결과로써, 황염과 청염 각각의 온도는 이산화탄소의 첨가에 따라 점차 낮아졌지만 황염과 청염의 경계온도는 거의 일정하였다. 산화제 측에 이산화탄소를 첨가함에 따라 상대적인 매연 농도는 낮아졌고 이는 산화제의 유속을 증가시켰을 때의 효과와 유사했다. 이것은 화염온도의 저하와 매연입자의 체류시간 감소에 기인하는 것으로 생각된다. 또한 이산화탄소의 첨가가 화염의 불안정성을 야기하여 순수 에틸렌/공기 화염에 비해 화염의 길이가 다소 증가하는 것으로 나타났다.

• 한국가스학회지
• /
• 제7권3호
• /
• pp.44-50
• /
• 2003

연료농도에 따른 대향류 화염구조의 변화를 조사하고 수치법을 검증하기 위해, 축대칭 메탄-공기 대향류화염을 모사하였다. 변형률 $a_g=20,\;60,\;90\;s^{-1}$과 연료 중 메탄의 몰분율 $x_m=20,\;50,\;80\%$를 수치매개변수로 하여, 변형율과 연료농도에 따라 온도분포, 닥트 중심축의 온도분포와 축방향 속도의 분포를 계산하였다. 축대칭 모사는 혼합분율 연소모델을 채용한 FDS로 수행하였고, 계산결과를 구체적 화학반응을 포함한 1차원 화염코드 OPPDIF의 계산결과와 비교하였다. 본 연구에서 조사한 모든 변형율과 연료농도에서 축대칭 모사의 온도 및 축방향 속도 분포가 1차원 계산결과와 잘 일치하는 것으로 나타났다. 연료농도가 증가하면 화염의 두께와 최고온도가 증가하고 반경이 감소함을 알 수 있었다.

• 한국해양공학회:학술대회논문집
• /
• 한국해양공학회 2002년도 춘계학술대회 논문집
• /
• pp.92-97
• /
• 2002

By changing the excess air ratio which affects strongly to the combustion characteristics, the flame stability range in the metal fiber burner were found and the range of the blue flame male and radiant mode were distinguished by direct photography. The results in our experiments for the flame stability zone were from a=1.4($354 KW/m^2$) to a=2.06($240 KW/m^2$), and then the blue flame mode zone was form a=1.87($266 KW/m^2$) to a=2.06($240 KW/m^2$) and the radiant mode one was form a=1.4($354 KW/m^2$) to a =1.78($278 KW/m^2$). And the flame was not fired when a is less than the lean condition a=2.45($202 KW/m^2$).

• 한국안전학회지
• /
• 제19권3호
• /
• pp.45-50
• /
• 2004

4-panel of 1m height and 45cm width were fixed on the $40cm{\times}40cm$ bottom plate and the opening of the panel comer was 5cm. Diameter of stainless vessel is loom and its height is 2cm and it located at the center of the bottom plate. 78mL liquid fuel was filled in the vessel and its depth was 1cm. Flame temperature was measured with K type thermocouple, and radiation heat of flame was measured with heat flux meter. Flame height and its behavior was visualized with video camera. and mass burning rate was measured by fuel combustion time. According to the development of fire, flame swirling was begin. From the experiment the mass burning rate was larger and the height of flame was higher than the usual pool fire flame. Flame temperature and heat flux also increased far more than the pool fire. Consequently the swirling air flow through the openings between the panel and thermal buoyance contribute to increase of heat release rate, flame length and mass burning rate.

• 대한기계학회논문집B
• /
• 제27권8호
• /
• pp.1089-1096
• /
• 2003

An experiment was performed to investigate lift-off, blow-off and combustion characteristics of a lifted coaxial diffusion flame according to fuel jet and air velocity. A jet diffusion flame which is attached on the nozzle rim begins to be lifted with increase of air velocity, and finally becomes blow-off at higher air velocity. In experiment, blow-off limit increased with increase of fuel jet velocity, however lift-off occurred at lower air velocity. Flame structure and combustion characteristics were examined by schlieren photos, temperature distributions and emission concentration distributions. Flame temperature became higher at midstream and its RMS became larger at up and downstream with increase of air velocity. Local NO concentration decreased but $CO_2$concentration increased with increase of air velocity, which shows combustion reaction becomes close to be stoichiometric at higher air velocity in spite of lift-off.