• 제목/요약/키워드: Counter Diffusion Flame

검색결과 12건 처리시간 0.03초

좁은 채널 내의 대향분류 메탄-공기 비예혼합 화염의 거동 특성 (Behavioral Characteristics of the Non-Premixed Methane-Air Flame Oppositely Injected in a Narrow Channel)

  • 윤영민;이민정;조상문;김남일
    • 대한기계학회논문집B
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    • 제33권4호
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    • pp.264-271
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    • 2009
  • Characteristics of a counter flowing diffusion flame, which is formulated by an oppositely-injected methane-jet flow in a narrow channel of a uniform air flow. The location of the flame fronts and the flame lengths were compared by changing the flow rates of fuel. To distinguish the effects of the narrow channel on the diffusion flame, a numerical simulation for an ideal two-dimensional flame was conducted. Overall trends of the flame behavior were similar in both numerical and experimental results. With the increase of the ratio of jet velocity to air velocity flame front moved farther upstream. It is thought that the flow re-direction in the channel suppresses fuel momentum more significantly due to the higher temperature and increased viscosity of burned gas. Actual flames in a narrow channel suffer heat loss to the ambient and it has finite length of diffusion flame in contrast to the numerical results of infinite flame length. Thus a convective heat loss was additionally employed in numerical simulation and closer results were obtained. These results can be used as basic data in development of a small combustor of a nonpremixed flame.

동축분류 층류제트 확산화염의 구조에 미치는 선회의 영향 (The Effect of Swirl on the Structure of Concentric Laminar Jet Diffusion Flame)

  • 김호영;민성기
    • 대한기계학회논문집
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    • 제16권3호
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    • pp.578-588
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    • 1992
  • 본 연구에서는 작은 층류화염을 형성하는 소형의 연소기에 대해 화염의 안정 화를 위하여 선회가 가해지는 등축분류 층류제트 확사화염의 구조에 미치는 선회의 강 도, 연료와 공기의 출구 레이놀즈 수, 연료와 공기의 선회방향의 영향등을 이론적인 모델의 구성과 수치실험을 통하여 고찰한다.

대향류 확산 화염 모델에서의 압력 및 산소분율에 따른 연소 특성 변화에 관한 수치해석 연구 (Numerical Study of Combustion Characteristics by Pressure and Oxygen Concentration in Counter-Flow Diffusion Flame Model)

  • 박진제;이영재
    • 청정기술
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    • 제27권1호
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    • pp.93-103
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    • 2021
  • 기후변화 대응과 탄소배출 저감에 대한 심각성 및 필요성이 중요시 되면서 세계 각국은 온실가스를 감축하고자 하는 노력을 지속하고 있다. 다양한 노력들 중 탄소기반 연료 사용 시 발생되는 이산화탄소를 포집하여 활용하는 CCUS에 대한 연구가 활발히 진행되고 있으며, 이러한 관점에서 CCUS와 함께 활용될 수 있는 가압 순산소 연소에 대한 연구도 여러 연구자들에 의해 진행되고 있다. 본 연구는 가압 순산소 연소의 화염 구조와 오염물질 배출과 관련된 기초적인 정보를 분석하는데 목적이 있다. 이를 위해 대향류 확산 화염 모델을 이용하여 압력 및 산소분율에 따른 연소의 특성을 분석한 결과, 압력이 높을수록 화학 반응의 활성화로 인한 반응율의 증가로 연소 온도가 증가하고 화염두께는 감소한 반면, 산소분율이 높을수록 반응율 증가 및 산화제 운동량 변화에 따른 확산의 영향으로 연소 온도 및 화염두께 모두 증가하였다. 이와 관련된 열방출 반응을 3가지 구간으로 구분하여 분석한 결과, 특히 산소분율이 증가할수록 산화제 측면에서 나타나는 화학 반응이 혼합분율에 따라 크게 두 개의 영역으로 세분화되는 특성이 나타났다. 또한, NO의 생성 메커니즘에 따라 구분된 배출지수(EINO)를 분석하였고, 각 해석 조건에 따른 NO의 생성 경향을 제시하였다.

Structural Characteristics of Turbulent Diffusion Flame Combusted with Simulated Coal Syngas

  • Park, Byung-Chul;Kim, Hyung-Taek;Chun, Won-Gee
    • 에너지공학
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    • 제11권4호
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    • pp.350-358
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    • 2002
  • The present work determined the flame structure characteristics of coal syngas combusted inside swirl burners with various nozzle types. Fuel nozzle types are largely classified into two groups of axial and tangential. Experiments were carried out for investigating the effects of fuel nozzle geometry, fuel composition ratio, heating rate, excess air, and degree of swirl on the turbulent diffusion flame structure. To determine the characteristics of the flame structure, axial type fuel nozzle diameter of laboratory-scale combustor is varied to 1.23, 1.96, and 2.95 ㎜ and the direction of tangential type nozzles are varied to radial, clockwise, and counter-clockwise. The comparison of the experimental results was performed to understand functional parameters relating the flame structure. Data analysis showed that the vertical straight flame height generally decreased with increasing swirl number and decreasing axial type nozzle diameter. Flame height established with tangential type nozzle is 3 times shorter than that with vertical type. The flame structures among the 3 different tangential fuel nozzles relatively showed no particular difference. By increasing the heating rate, the width of flame increased generally in both vertical and tangential flame. Within the present experimental parameters of the investigation, flame structure is mainly depends on the nozzle type of the combustor. The visually investigated flame lengths are confirmed through the analysis of temperature profile of each flame.

대향류 확산화염에 대한 직접수치모사의 검증 (An Evaluation of a Direct Numerical Simulation for Counterflow Diffusion Flames)

  • 박외철
    • 한국안전학회지
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    • 제16권4호
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    • pp.74-81
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    • 2001
  • A direct numerical simulation (DNS) was applied to nonpremixed counter-flow diffusion flames between oxidizer and fuel ducts. The objective of this study is to evaluate the numerical method for simulation of axisymmetric counterflow diffusion flames. Effects of computational domain size and grid size were scrutinized, and then the method was applied to air-methane diffusion flames. The results at zero gravity conditions were in good agreement with those obtained by the one-dimension flame code OPPDIF. It was confirmed thai the numerical method is applicable to the diffusion flames at the normal gravity conditions since the results clearly showed the effects of buoyancy and velocity ratio.

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산화제 제어 확산화염의 화염구조 및 NO 생성 특성에 관한 수치해석적 연구 (Numerical Study on Flame Structure and NO Formation Characteristics in Oxidizer-Controlled Diffusion Flames)

  • 이창언;한지웅
    • 대한기계학회논문집B
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    • 제26권5호
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    • pp.742-749
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    • 2002
  • Numerical Study with detailed chemistry has been conducted to investigate the flame structure and NOx formation characteristics in oxygen -enhanced(CH$_4$/O$_2$-$N_2$) and oxygen-enhanced-EGR(CH$_4$/O$_2$-$CO_2$) counter diffusion flame with various strain rates. A small amount of $N_2$is included in oxygen-enhanced-EGR combustion, in order to consider the inevitable $N_2$contamination by $O_2$production process or air infiltration. The results are as follows : In CH$_4$/O$_2$-$CO_2$flame it is very important to adopt a radiation effect precisely because the effect of radiation changes flame structure significantly. In CH$_4$/O$_2$-$N_2$flame special strategy to minimize NO emission is needed because it is very sensitive to a small amount of $N_2$. Special attention is needed on CO emission by flame quenching, because of increased CO concentration. Spatial NO production rate of oxygen-enhanced combustion is different from that of air and oxygen-enhanced-EGR combustion in that thermal mechanism plays a role of destruction as well as production. In case CH$_4$/O$_2$-$CO_2$flame contains more than 40% $CO_2$it is possible to maintain the same EINO as that of CH$_4$/Air flame with accomplishing higher temperature than that of CH$_4$/Air flame. EINO decreases with increasing strain rate, and those effects are augmented in CH$_4$/O$_2$flame.

부력을 최소화한 대향류 확산화염 소화거동에서 연료농도구배의 영향 (Influence of Fuel concentration gradient on the Extinction Behavior in Buoyancy minimized Counterflow Diffusion Flame)

  • 박진욱;박정;윤진한;길상인
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.379-381
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    • 2014
  • Influence of fuel concentration gradient was investigated near flame extinction limit in buoyancy-suppressed non-premixed counterflow flame with triple co-flow burner. The use of He curtain flow produced a microgravity level of $10^{-2}-10^{-3}g$ in He-diluted non-premixed counter triple co-flow flame experiments. Flame stability map was presented based on flame extinction and oscillation near extinction limit. The stability map via critical diluent mole fraction with global strain rate was represented by varying outer and inner He-diluted mole fractions. The flame extinction modes could be classified into five: an extinction through the shrinkage of the outmost edge flame forward the flame center with and without self-excitation, respectively ((I) and (II)), an extinction via the rapid expansion of a flame hole while the outmost edge flame is stationary (III), both the outermost and the center edge flames oscillate, and then a donut shaped flame is formed or the flame is entirely extinguished (IV), a shrinkage of the outermost edge flame without self-excitation followed by shrinking or sustain the inner flame (V).

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에틸렌 확산화염 내 질소 혼합이 매연 생성 특성에 미치는 영향 (Effect of N2 Diluent on Soot Formation Characteristics in Ethylene Diffusion Flames)

  • 김준수
    • 해양환경안전학회지
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    • 제29권4호
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    • pp.356-362
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    • 2023
  • 기후 변화에 따른 위험성은 전 세계적으로 오랜 기간 강조되고 있으며, 이를 극복하기 위한 노력은 해운분야에서도 국제해사 기구를 중심으로 이어지고 있다. 연소과정에서 발생한 매연을 제어하기 위하여 매연 생성 특성에 관한 연구는 필수적이다. 본 연구에서는 에틸렌 가스를 기반으로 한 대향류 확산화염에서 불활성 기체인 질소를 혼합하여 화염온도, 화염형태, 매연 생성 관련된 화학종의 상태변화를 확인하기 위해 광소멸법과 화학반응 수치해석을 수행하였다. 연구 결과. 질소의 혼합비율이 증가함에 따라 화염온도 감소와 매연체적분율 감소로 이루어졌다. 매연 입자가 분포하는 구간도 감소하였으며, 30% 이상 혼합비율이 높아지면 체적분율 감소율이 감소하였다. 매연 성장에 관여하는 화학종들의 몰분율도 감소하였다. HACA 반응 관련 화학종은 탄화수소 연료 비율에 따라 영향을 받으나, 홀수탄소 경로 관련 화학종은 탄화수소 연료 비율뿐만 아니라 화염온도 영향을 받는 것을 확인하였다.

산화제 제어 화염의 구조 및 NO 생성 특성 (Structure and NO formation characteristics of oxidizer-controlled diffusion flames)

  • 한지웅;이창언
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.185-190
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    • 2001
  • Numerical Study with detailed chemistry has been conducted to investigate the flame structure and NOx formation characteristics in oxygen-enhanced$(CH_4/O_2-N_2)$ and oxygen-enhanced-EGR$(CH_4/O_2-CO_2)$ counter diffusion flame with various strain rates. A small amount of $N_2$ is included in oxygen-enhanced-EGR combustion, in order to consider the inevitable $N_2$ contamination by $O_2$ production process or air infiltration. The results are as follows : In $CH_4/O_2-CO_2$ flame it is very important to adopt a radiation effect precisely because the effect of radiation changes flame structure significantly. In $CH_4/O_2-N_2$ flame special strategy to minimize NO emission is needed because it is very sensitive to a small amount of $N_2$. Special attention is needed on CO emission by flame quenching, because of increased CO concentration. Spatial NO production rate of oxygen-enhanced combustion is different from that of air and oxygen-enhanced-EGR combustion in that thermal mechanism plays a role of destruction as well as production. In case $CH_4/O_2-CO_2$ flame contains more than 40% $CO_2$ it is possible to maintain the same EINO as that of $CH_4/Air$ flame with accomplishing higher temperature than that of $CH_4/Air$ flame. EINO decreases with increasing strain rate, and those effects are augmented in $CH_4/O_2$ flame. Complementary study is needed with extending the range of strain rate variation.

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둔각 물체를 이용한 엔진 나셀 화재 소화 특성 (The Characteristic of Extinguishment of Engine Nacelle Fire Using a Bluff Body)

  • 이정란;이의주
    • 한국안전학회지
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    • 제27권1호
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    • pp.20-25
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    • 2012
  • The purpose of the study is to assess the extinguishing concentration of inert gases in engine nacelle fire. The experiment was performed with a two dimensional rectangular bluff body stabilized flames, where the fuel was ejected to counter flow and co-flow against an oxidizer stream. Two inert gases, $CO_2$ and $N_2$, were used for extinguishing agent in the oxidizer and methane was used for fuel. The main experimental parameters were the direction of injecting fuel, the kinds of agent and the velocity ratio between air and fuel streams, which controlled the mixing characteristic near bluff body and the strength of recirculation zone in the downstream. The result shows the flame structure and the mode were strongly dependent with fuel/air ratio and the fuel jet direction. For both flow configurations, the extinguishing concentration of $CO_2$ was smaller than the $N_2$ because of the large heat capacity of $CO_2$. However, the concentration of inert gasesat blowout was much smaller than those in the cup burner and coflow jet diffusion flames, which implies that the extinction mechanism of bluff body stabilized flames was mainly due to the aerodynamic aspect. Compared to co-flow fuel injection, the extinguishing concentration of inert gases under counter flow configuration was lower. The effect of direction might result from the mixing characteristic and strength of recirculation zonearound a bluff body. More details should be investigated for the characteristic of recirculation zone in the wake of bluff body using the LES(Large Eddy Simulation).