• 제목/요약/키워드: Fuel-rich Combustion

검색결과 178건 처리시간 0.023초

150kW급 열병합발전 하이브리드 시스템 최적화 연구 (Optimization of 150kW Cogeneration Hybrid System)

  • 최재준;김혁주;정대헌;박화춘
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 동계학술발표대회 논문집
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    • pp.340-344
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    • 2008
  • The importance of the more efficient cogeneration system is emphasized. Also the more clean energy is needed at recent energy system. The cogeneration system using Lean burn engine is more preferred to the system using Rich burn engine because of the electrical efficiency. Although the cogeneration system using Lean burn engine is economically preferred, because of the NOx emission level, the system using Rich burn engine with 3-way catalyst can only be used in Korea. The NOx regulation level is 50ppm at oxygen level 13%. The cogeneration hybrid system using Lean burn engine is up to be optimized because of the large amount of the extra-fuel at the after-burner system. The after-burner system at different concept was applied. The reduction time for the activation temperature of the DeNOx catalyst was achieved by making a hole between the combustor and boiler. Because of the lowered fuel consumption, the lowered temperature level was optimized by blocking the hole of the boiler The optimized cogeneration hybrid system consumes $76Nm^3/h$ LNG to produce 150kW electricity compared to before optimization $103Nm^3/h$ LNG. The system was accurately evaluated and the result is following ; 90% total efficiency, below 10 ppm NOx, 50ppm CO, 25ppm HC. The cogeneration hybrid system can meet the current NOx level and exhaust gas regulation. It can achieve the clean combustion gas and efficient cogeneration system.

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EMISSION ANALYSIS OF A MEDIUM CAPACITY DIESEL ENGINE USING MAHUA OIL BIODIESEL

  • Sharma, Ajay Kumar;Das, L.M.;Naik, S.N.;Chauhan, Bhupendra Singh;Cho, Haeng Muk
    • 에너지공학
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    • 제22권2호
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    • pp.136-140
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    • 2013
  • The stringent emission norms cannot be met through engine design and exhaust after treatment alone. Use of oxygenated fuel like biodiesel as a alternative to diesel may be the best way to reduce emissions today. In this study, Diesel fuel and pure biodiesel (mahua oil) were tested on a single cylinder naturally-aspirated direct-injection diesel engine. The study aims to investigate the effects of the mahua oil biodiesel on existing diesel engine emissions. The effect of test fuels on engine emissions like CO, HC, $CO_2$, NOx and smoke emissions was investigated with respect to the load on engine. Smoke opacity of Diesel engine was lower in case of biodiesel of mahua oil as compare to mineral diesel. NOx emissions was little higher during the whole range of loading, which is a typical characteristic of biodiesel. However the increments are within in the narrow range. $CO_2$ emissions was bit higher which is the indication of better combustion due to presence of rich oxygen in the mixture, it results in the low values of CO and HC during the whole range of experiments. Thus considering environmental norms most of the engine emissions, it can be concluded and biodiesel derived from mahua oil could be used in a conventional diesel engine without any modification.

정상초음파가 개재하는 메탄/공기 및 프로판/공기 예혼합화염의 동역학적 특성 비교 (Comparison of Dynamic Characteristics of Methane/Air and Propane/Air Premixed Flames with Ultrasonic Standing Wave)

  • 김민철;배대석;김정수
    • 한국추진공학회지
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    • 제21권4호
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    • pp.44-51
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    • 2017
  • 정상초음파가 개재하는 탄화수소계 연료공기 예혼합화염의 동역학적 특성 비교에 대한 실험적 연구결과를 제시한다. 전파화염의 이미지는 고속카메라를 이용하여 획득하였으며, 이미지 후처리를 통해 메탄/공기와 프로판/공기 예혼합화염의 화염거동을 상세히 관찰하였다. 이론당량비 이하의 연료희박조건에서 정상초음파 개재에 의한 연소반응 촉진으로 인해 화염전파속도는 증가되었다. 한편, 당량비가 1.2인 메탄/공기 화염과 당량비 1.4 이상의 프로판/공기 화염의 전파속도에 대한 초음파의 영향은 연료희박조건과 반대되는 결과를 보였다.

더스트 클라우드 내에서의 화염 진행과 연소 한계 (Flame Propagation in Dust Cloud and its Flammability Limits)

  • 문인상;윤영빈;김문기;조태영
    • 한국연소학회:학술대회논문집
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    • 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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    • pp.201-208
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    • 2003
  • Wheat dust cloud를 $5{\times}5{\times}214.1cm^3$ square tube내부에 발생시켜 화염의 전달과 연소 한계에 관한 연구를 수행하였다. 사용된 미립자는 $160{\mu}m-300{\mu}m$의 크기로 분류되어 주로 사용되었고 $300{\mu}m-325{\mu}m$크기의 미립자가 더불어 사용되었다. 연소 튜브는 연료로 사용되는 미립자를 튜브의 상단에서부터 컨베이어 벨트를 사용해서 공급받아 튜브의 하단에서 전기코일을 사용하여 점화시키는 구조로 고안되었다. 화염의 최대 진행속도는 작은 크기와 보다 큰 크기의 미립자를 사용했을 때가 각각 523cm/sec와 373cm/sec로 측정되었다. 연소 속도는 입자의 크기와 집접도(concentration)에 따라 변화를 보였는데 최소 3cm/sec에서 최대 7.5cm/sec로 관측되었다. 그러나 화염의 두께는 놀랍게도 입자의 집접도와 큰 연관이 없어 보였는데, 이는 앞으로도 보다 많은 연구를 통한 검증이 필요하리라 생각된다. 끝으로 fuel rich flammability는 $790g/m^3$으로 stoichiometric mixture $230g/m^3$에 비교해 월등히 높은 값으로 관측되었다.

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CMC model에 의한 near-extinction methane/air turbulent jet diffusion flame의 수치적 모사 (Numerical Study on Methane/Air Turbulent Jet Diffusion Flames Near-Extinction Using Conditional Moment Closure Model)

  • 강승탁;김승현;허강일
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2002년도 제25회 KOSCI SYMPOSIUM 논문집
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    • pp.11-17
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    • 2002
  • The first-order conditional moment closure (CMC) model is applied to $CH_4$/Air turbulent jet diffusion flames(Sandia Flame D, E and F). The flow and mixing fields are calculated by fast chemistry assumption and a beta function pdf for mixture fraction. Reacting scalar fields are calculated by elliptic CMC formulation. The results for Flame D show reasonable agreement with the measured conditional mean temperature and mass fractions of major species, although with discrepancy on the fuel rich side. The discrepancy tends to increase as the level of local extinction increases. Second-order CMC may be needed for better prediction of these near-extinction flames.

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추력 30톤급 액체산소/케로신 로켓엔진 연소장치 개발(II)-가스발생기 (Development of 30-Tonf LOx/Kerosene Rocket Engine Combustion Devices(II) - Gas Generator)

  • 최환석;서성현;김영목;조광래
    • 한국항공우주학회지
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    • 제37권10호
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    • pp.1038-1047
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    • 2009
  • 추력 30톤급 펌프공급방식 액체로켓엔진을 위한 가스발생기 개발 과정에 관하여 기술하였다. 액체산소와 케로신을 추진제로 연료 과농 조건에서 작동하는 가스발생기의 개발을 위해 분사기 개발에서부터 시작하여 축소형, 실물형 개발시제를 거쳐 가스발생기 단품 개발을 성공적으로 완료하였다. 가스발생기 설계 과정에서 다양한 해석적 방법을 적용하였으며 점화 시험, 연소성능 및 연소안정성 평가시험, 내구성 평가시험 등을 통해 가스발생기의 성능요구사항을 시험적으로 검증하였다. 개발된 가스발생기는 연소압 및 혼합비 운용 영역 내에서 안정적으로 작동하며 성능 및 수명 요구조건을 만족시킴을 확인하였다.

THE MORPHOLOGY OF CHROMIUM AND LIF MEASUREMENT OF ATOMIC ARSENIC IN LAMINAR DIFFUSION FLAMES

  • Yoon, Young-Bin
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 1997년도 제15회 KOSCO SYMPOSIUM 논문집
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    • pp.61-68
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    • 1997
  • The morphology and size distribution of chromium oxides and the concentration measurement of atomic arsenic have been studied in laminar diffusion flames. Nitrogen was added to vary flame temperatures in hydrogen flames. Ethene flames were used in order to investigate the potential for interaction between the soot aerosol that is formed in these flames and the chromium aerosol. Two sources of chromium compounds were introduced: chromium nitrate and chromium hexacarbonyl. A detailed investigation of the morphology was carried out by scanning electron microscopy (SEM). The amounts of Cr(VI) and total Cr were determined by a spectrophotometric method and by X-ray fluorescence spectrometry, respectively. Also, LIF was used for the measurement of atomic arsenic, which was excited at 197.2 nm and was detected at 249.6 nm. Results showed that the morphology of the particles varied with the flame temperature and with the chromium source. The particles were characterized by porous structures, cenospheres and agglomerated dense particles when chromium nitrate solution was added to the flames. At low to moderate temperatures, porous sintered cenospheric structures were formed, in some cases with a blow hole. At higher temperatures, an agglomerated cluster which was composed of loosely sintered submicron particles was observed. It was also found that the emission of Cr(VI) from the undiluted $H_2$ flame was more than 10 times larger than in the 50% $H_2$ / 50% $N_2$ flame on a mass basis. Single point LIF measurement of atomic arsenic indicated that arsenic exist only in the low temperature, fuel rich region.

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메탄의 무촉매 부분산화를 통한 합성가스 제조 연구 (A Study on Syngas Production By Noncatalytic Partial Oxidation of Methane)

  • 나익환;양동진;채태영;;방병열;양원
    • 한국수소및신에너지학회논문집
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    • 제20권4호
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    • pp.337-343
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    • 2009
  • Noncatalytic partial oxidation of methane for producing synthesis gas was studied in a lab-scale experimental apparatus. Partial oxidation developed for high-temperature, fuel-rich combustion and it is exothermic process. but Steam reforming and Caron reforming is highly endothermic process to need much energy. Noncatalytic partial oxidation of methane is affected by temperature and equivalent ratio, so we studied effect about composition of synthesis gas at lab scale reactor. We used electronic heater to control the temperature of reactor. The quality of synthesis gas is improved and reduced heat value to require at Noncatalytic partial oxidation because the reacting temperature is lower at oxy condition.

코크스 오븐 가스(COG)를 이용한 수소 및 합성가스 제조 기술 개발 동향 분석 (A Review of Technology Development Trend for Hydrogen and Syngas Production with Coke Oven Gas)

  • 최종호
    • 한국산업융합학회 논문집
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    • 제25권6_3호
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    • pp.1247-1260
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    • 2022
  • The steel industry accounts for about 5% of the total annual global energy consumption and more than 6% of the total anthropogenic carbon dioxide emissions. Therefore, there is a need to increase energy efficiency and reduce greenhouse gas emissions in these industries. The utilization of coke oven gas, a byproduct of the coke plant, is one of the main ways to achieve this goal. Coke oven gas used as a fuel in many steelmaking process is a hydrogen-rich gas with high energy potential, but it is commonly used as a heat source and is even released directly into the air after combustion reactions. In order to solve such resource waste and energy inefficiency, several alternatives have recently been proposed, such as separating and refining hydrogen directly from coke oven gas or converting it to syngas. Therefore, in this study, recent research trends on the separation and purification of hydrogen from coke oven gas and the production of syngas were introduced.

한국형발사체 3단 터빈배기부 개념설계 (Conceptual Design of Turbine Exhaust System for 3rd stage of Launch Vehicle)

  • 신동순;김경석;한상엽;방정석;김현웅;조동혁
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.1068-1071
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    • 2017
  • 3단 터빈배기부 구성은 터빈 플랜지, 열교환기, 배기덕트와 추력노즐로 이루어진다. 냉가스 가압 방식에 비하여 열교환기 가압 방식을 사용함으로서 추진제탱크 가압을 위한 헬륨가스 자체 무게와 저장 탱크 무게가 감소하는 장점이 있기 때문에 발사체에 열교환기를 사용한다. 가스발생기는 추진제 연료과농 조건에서 연소가 이루어지며, 연소가스 중에 그을음이 많이 포함되어 있기 때문에 열교환 효율이 감소하는 것을 고려하여 열교환기를 설계해야 한다. 본 논문에서는 터빈배기부 구성품 배치, 열교환기 내부 구조 및 제작성을 고려한 설계기법, 기 설계된 노즐 설계를 바탕으로 3단 터빈배기부 재 노즐 설계 형상에 대한 장점을 기술하였다.

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