• 제목/요약/키워드: Oxidizer-Controlled Flame

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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.

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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하이브리드 로켓의 산화제 종류에 따른 고체연료 연소특성 비교 (Comparison of Combustion Characteristic with GN2O and GOX as Oxidizer in Hybrid Rocket)

  • 이정표;조성봉;김수종;윤상규;박수향;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
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    • pp.223-227
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    • 2006
  • 하이브리드 추진 시스템에서의 산화제 종류에 따른 연소특성을 알아보기 위한 연구를 수행하였다. 산화제는 $GN_2O$와 GOX를 사용하고, 고체연료는 폴리에틸렌(PE)을 사용해 연소시험을 하였다. 산화제 종류에 따른 연소특성은 O/F 비에 따른 화염온도로 해석이 가능하였으며, $GN_2O$가 GOX보다 하이브리드 추진 시스템의 산화제로 효율이 좋음을 확인하였다 산화제의 유량은 직경이 다른 여러 개의 쵸킹 오리피스로 제어했고, 산화제 공급 유량범위는 $0.0138{\sim}0.0427kg/sec$ 이었다. 산화제 종류에 따른 연소특성을 표현하는 실험식은 고체연료의 질량유속으로 나타냈고, 이는 물질전달 수와 산화제의 질량유속으로 얻어진다.

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In-Situ TEM Observation on Phase Formation of $TiO_2$ Nanoparticle Synthesized by Flame Method

  • Jie, H.S.;Park, H.;Kim, K.H.;Ahn, J.P.;Park, J.K.
    • 한국분말야금학회:학술대회논문집
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    • 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part 1
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    • pp.469-470
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    • 2006
  • [ $TiO_2$ ] nanoparticle was synthesized by the flame method, which was controlled by varying the ratio and flow rate of gas mixtures consisting of oxygen (oxidizer), methane (fuel) and nitrogen (carrier gas). The crystalline phases of $TiO_2$ nanoparticle depended strongly on the temperature distribution in the flame, whereas the morphology was not sensitive. We proved that the anatase phase formed without the phase transformation in the flame and the rutile phase generated through several phase transformations.

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로켓 산화제 과잉 예연소기용 분사기의 고압 분무특성 연구 (Spray Characteristics of the Oxidizer-rich Preburner Injector in High Pressure Environments)

  • 양준호;최성만
    • 한국추진공학회지
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    • 제12권2호
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    • pp.48-56
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    • 2008
  • 액체로켓 예연소기의 산화제 과잉 연소는 매우 어려운 과업이다. 이를 위해서는 작동 조건에서 좋은 혼합특성을 갖는 분사기를 설계하는 것이 무엇보다 중요하다. 따라서 고압환경에서 로켓 산화제 과잉 예연소기용 분사기의 분무특성을 실험을 통해 알아보았다. 분사기는 연료 및 산화제 오리피스, 산화제 스커트로 구성되어있다. 분사기의 분무특성을 알아보기 위해 주위기체압력을 0에서 30kgg/cm2[g]까지 가압하여 분무 가시화, Sauter 평균 입경을 측정하였으며, 액적 크기는 이미지 처리 기법을 이용하였다. 실험결과로부터 로켓 산화제 과잉 예연소기용 분사기의 분무특성을 이해할 수 있었으며, 로켓 산화제 과잉 예연소기 개발에 중요한 자료로 활용될 수 있을 것이다.

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).