• Title/Summary/Keyword: 최연소

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3-Dimensional Model for Pulverized Coal Combustion (미분탄 연소로의 난류 유동장 및 반응장 해석을 위한 3차원 모델)

  • 이경옥;서경원;최병선
    • Journal of Energy Engineering
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    • v.1 no.1
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    • pp.76-86
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    • 1992
  • A three-dimensional model has been developed for pulverized coal combusters and gasifiers. Coal devolatilization, heterogeneous char oxidation, gas particle interchange, radiation, gas phase oxidation, primary and secondary stream mixing, and heat losses are considered. A finite difference method was used to solve the ordinary non-linear differential equations. The effects of primary and secondary stream flow ratio and coal particle size are investigated.

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Numerical Study of Flame Stability of Turbulent Combustion in a Dual Combustion Ramjet (이중연소 램제트 엔진의 난류 연소 현상과 화염 안정성)

  • Choi, Jeong-Yeol;Han, Sang-Hoon;Kim, Kyu-Hong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.371-374
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    • 2011
  • High-resolution numerical study is carried out to investigate the flame stability of the turbulent supersonic combustion in a Dual-Combustion Ramjet (DCR). The auto-ignition in a shear layer between hydrogen/carbon-monoxide syngas and air was studied at elevated enthalpy condition. Comparison of a constant area combustor and a combustor with a small divergence angle shows that the supersonic combustion has a characteristics of the lifted flame and its stability is influenced significantly by the compressibility.

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Unsteady Combustion Phenomena in Scramjet Combustor (스크램제트 연소기의 비정상 연소현상)

  • Choi Jeong-Yeol
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.364-367
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    • 2005
  • A series of computational simulations have been carried out for non-reacting and reacting flows in channel-type and divergent scramjet combustor configurations with and without a cavity. Transverse injection of hydrogen is considered with the injection pressure varying from 0.5 to 1.5 MPa. The detailed resolution of the oscillatory flow and flame dynamics are captured at sufficient scale to identify the underlying physical mechanisms, and the role of combustor configuration, cavity and amount of heat addition could be understood.

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Studies on NOx reduction by two-staged combustion and characteristics of N-release in pulverized coal combustion (탄연소시 N-release특성과 2단연소에 의한 NOx 저감에 관한 연구)

  • Hahn, Woong;Park, Chu-Sik;Kim, Sung-One;Choi, Sang-Il
    • 한국연소학회:학술대회논문집
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    • 2000.05a
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    • pp.45-56
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    • 2000
  • 미분탄 연소시 발생하는 질소산화물(NOx)은 석탄의 형태 및 등급에 따라 다르게 나타난다. 석탄에 함유되어 있는 질소 성분은 준역청탄인 경우 촤보다 휘발분에 많이 분포되어 있으며, 역청탄인 경우 촤에 많이 분포되어 있음을 확인하였다. 석탄에 함유되어 있는 질소의 분포에 따라 연속과정에 의해 최대로 발생할수 있는 질소산화물의 양과 질소산화물로 전환되는 정도를 예측할 수 있었다. NOx 방출은 석탄중에 함유되어 있는 질소성분의 양에 영향을 받으며, 고온 노출 시 방출되는 휘발성분의 양의 증가 그리고 공기비를 감소함으로서 질소산화물의 저감율을 증가시킬 수 있었다. 특히 질소산화물의 환원은 연료가 풍부한 조건에서 연소초기 고온으로 연소하는 경우 효과적이었다. 또한 2단 연소에 의한 방법으로 1단에서는 저공기비로 유지하고 2단에서 추가적인 공기를 공급함으로서 최종 공기비는 1.2인 조건에서 효과적으로 NOx를 저감할 수 있었다.

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Study on the Combustion Performance Estimation of Hydrazine Mono Propellant Thruster (하이드라진 단일 추진제 추력기의 연소 성능예측에 관한 연구)

  • 정인석;윤영빈;최정열;김철중;명대근;정기훈
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.04a
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    • pp.30-30
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    • 1998
  • 다목적 실용위성의 자세 제어용으로 장착되는 하이드라진 단일 추진제 추력기의 연소성능 특성을 살펴보았다. 일차적으로, 연소기내의 화학 평형 계산을 통하여 하이드라진 연소 생성물인 암모니아의 분해율과 초기 엔탈피 수준에 따른 추력기의 성능 특성을 살펴보았다. 다음 순서로, 연소기 내의 비평형 화학 반응 계산을 통하여 연소진행 시간에 화학 조성 및 성능 특성을 살펴 볼 수 있었으며, 최종적으로, 점성 및 비점성, 동결 및 비평형 화학 반응 해석에 따른 성능 특성 변화를 살펴보았다. 본 연구 결과로부터 각 작동 변수에 따른 추격기 성능 특성의 변화를 이해할 수 있었으며, 이는 단일 추진제 추력기 연소실의 구성, 설계 및 추력기의 운용 조건 설정에 중요한 자료로 이용될 수 있을 것으로 기대된다.

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Combution characteristics analysis of partition materials on public toilets (공공화장실 칸막이 재료의 연소특성 분석)

  • Chae, Hak-Byeong;Min, Jeong-Gi;Lee, Sang-Gwon;Jeong, Guk-Sam;Won, Jeong-Hun
    • Proceedings of the Korea Institute of Fire Science and Engineering Conference
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    • 2013.11a
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    • pp.178-179
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    • 2013
  • 본 연구에서는 현재 사용되고 있는 건축물 내의 화장실 칸막이 재료를 대상으로 ISO 5660-1 콘칼로리미터(Cone calorimeter) 실험을 실시하여 대상 실험 재료들의 연소 특성을 비교 평가 하였다. 모두 5종류의 실험체를 사용하였으며, 화재 발생시 연소 중요 평가항목인 착화시간(Time to ignition), 총 방출열량(Total heat release), 최고 열방출율(Peak heat release rate), 평균 열방출율(Mean heat release rate)을 중점적으로 평가하였다. 실험결과, 착화시간은 일반 합판패널에서 빠르게 일어났으며, 총 방출열량, 최고 열방출율, 평균 열방출율은 고밀도 압축패널에서 높게 나타난 것으로 분석되었다.

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Simultaneous NOx, PM Reduction by the Late Injection & Fast Combustion Type Premixed Combustion Technology (지연분사급속연소방식 예혼합연소 기술에 의한 NOx, PM의 동시저감)

  • 김장헌;최인용;김창일
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.4
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    • pp.31-35
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    • 2004
  • A new combustion strategy called LIFC(Late Injection & Fast Combustion) was developed for simultaneous reduction of particulate matter(PM) and nitrogen oxides(NOx) in exhaust emission of diesel engines, In this study, effects of injection timing and injection pressure under relatively high EGR rate were investigated. The experiments were conducted in a conventional engine over a range of commercial engine speed. The test engine could be operated in LIFC up to 2000rpm / bmep 5 bar condition with significant reduction of NOx and PM. The experimental results showed potential for the mechanism of the simultaneous reduction of NOx and PM from HSDI diesel engines.

Numerical Analysis of Turbulent Combustion of a Kerosene/Oxygen Coaxial Injector with a Recess (리세스가 있는 케로신/산소 동축 분사기의 난류 연소 유동 해석)

  • Choi, Jeong-Yeol;Shin, Jae-Ryul
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.77-78
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    • 2011
  • A multi-step quasi-global mechanism is developed for the kerosene/oxygen combustion analysis including dissociation products. Reaction constants of the global reaction are determined to have agreement with experimental data. The mechanism is used for the numerical analysis of the combustion flow field of the kerosene/oxygen shear coaxial injector. The results from high-resolution numerical analysis confirmed qualitatively that the recess enhance the fuel/air mixing and combustion efficiency by the increased flow instabilities.

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A Study on Combustion Patterns of Flammable Liquids by Contained Oil Test (담유 실험에 의한 인화성 액체의 연소 패턴 해석에 관한 연구)

  • Joe, Hi-Su;Choi, Chung-Seog
    • Fire Science and Engineering
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    • v.28 no.4
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    • pp.14-20
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    • 2014
  • The purpose of this study is to analyze combustion patterns by filling a specific container with a flammable liquid and performing combustion tests in a divided space. The container used for the test is made of plastic, 20 mm in depth and 150 mm in width. After the liquid was ignited, its combustion process was photographed using a digital camera and video camera. It was found that in the case of benzene, the flame reached its peak at the fastest speed about 60 s while in the case of alcohol, the flame reached its peak at the lowest speed about 360 s, which is approximately six times slower than the benzene. In most cases, when the flame reached its peak, smoke generated was dark as the plastic container and flammable liquid were combusted simultaneously. After completion of the combustion, it was possible to sample oil vapor from all flammable liquids excluding soybean oil as a result of the examination of oil vapor using a crime investigation tube. That is, it can be seen that there is significant difference in flame propagation speed, pattern, etc., depending on the combustible substances.