• Title/Summary/Keyword: Gas Combustion

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Diode-Laser Absorption Sensors for measurement of combustion Gas (연소배기 가스의 계측을 위한 다이오드 레이저 센서)

  • Shin, Myung-Chul;Kim, Se-Won;Kim, Dong-Hyuck
    • Journal of the Korean Society of Combustion
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    • v.11 no.3
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    • pp.26-35
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    • 2006
  • This work forcus on the development of gas sensor that measure the concentrations of exhaust gas using diode laser, Each diode laser for exhaust gas measurement is set to work at near-IR using both DA and WMS methods. Also use of fiber-coupled optical elements makes such a sensor rugged and easy to align. The results showed that gas concentrations of $O_2$, CO, $CO_2$, NO are accurately measured within ${\pm}2%$ error. The application of WMS method increased the beam intensity 2-3 times higher than DA method. It were experimentally compared WMS (Wavelength Modulation Spectroscopy) with DA (Direct Absorption) for the accuracy.

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Exhaust Emissions Characteristics on the SI Engine according to the Air-Fuel Mixture with Ozone (혼합기 오존 첨가에 따른 SI기관의 배기배출물 특성)

  • Lee, B.H.;Yi, C.S.;Lee, Y.H.;Lee, C.K.;Jeong, H.M.;Chung, H.S.
    • Journal of Power System Engineering
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    • v.10 no.3
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    • pp.5-10
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    • 2006
  • In a conventional and lean operating engine, the state of mixture is very important in the combustion and emission characteristics. Lean operation is known to decrease the formation while maintaining a good fuel economy, but the unstable operation due to misfire and erratic combustion prevents engines from being operated at very lean mixtures, so both combustion rates and exhaust emission formation need to be satisfied comparably. In this study, it is designed and experimented the modified engine, and analyzed the combustion and exhaust emission according to the change of engine speed and with adding ozone. The conclusions were drawn out and enumerated as follows. 1. At the experimental result of automobile diesel engine, it has been verified that the formation of particulate matter(PM) gas is able to be lower with the addition of optimum quantities of ozone. 2. Carbon monoxide(CO) was formed by the lack of oxygen and the thermal dissociation in the combustion process. Therefore, with the change of swirl valve's position and addition of oxygen and ozone, CO formation was decreased by the increasing of excessive O2, but it was increased by the temperature of combustion gas growing higher. As a result of the two effects, CO formation was decreased in this study. 3. Hydrocarbon(HC) was formed by the lack of O2, and the flow of mixture in cylinder. According to opening of the swirl valve and adding the oxygen and ozone, hydrocarbon gas was decreased by 20%, 9%, and 27.5%, respectively. 4. Nitric oxides($NO_x$) was strongly affected by the combustion gas temperature. As a result of respectively experimental conditions, $NO_x$ formation was increased about 20% due to (be the) high(er) combustion gas temperature.

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The Pollutant Emissions Characteristics of Lean-Rich Combustion System with Exhaust Gas Reciculation (EGR 시스템을 적용한 린-리치 연소시스템의 공해물질 배출 특성 연구)

  • Oh, Wheesung;Yu, Byeonghun;Kim, Jong-Hyun;Lee, Chang-Eon
    • 한국연소학회:학술대회논문집
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    • 2014.11a
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    • pp.233-234
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    • 2014
  • Lean-rich combustion system was composed both fuel-lean and fuel-rich flame at once. Each of fuel-lean and fuel-rich combustion types to reduce Thermal $NO_x$ and obtain flame stability. This study was confirmed a stability of flame through variation of flame shape that EGR was applied and compared the emission characteristics of EGR lean-rich combustion system to normal premixed combustion system at real condition to review a utility of the system. As a result, emission index of $NO_x$ and CO generated from EGR lean-rich combustion system at global equivalence ratio is 0.85 just half level($NO_x$ 0.31 g/kg, CO 0.08g/kg) compared to the amount generated from normal premixed combustion system at equivalence ratio is 0.78.

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Combustion Characteristics and Application of Cyclon Combustor

  • Chae, J.O.;Xu, F.Z.;Yu, J.;Moon, S.I.;Kim, K.Y.
    • 한국연소학회:학술대회논문집
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    • 2001.06a
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    • pp.82-89
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    • 2001
  • This paper concerns lean gas cyclone combustion system adopting distributed inlets with different velocity to promote ignition and burnout properties. Detailed temperature measurements have been achieved under different operating conditions and flue gas compositions and NOx have been measured. Experimental results show that cyclone combustor provided increasing combustion stability and reduction NOx emission level to negligible level.

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CFD STUDY ON THE COMBUSTION CHAMBER OF AN OXY-FUEL FGR BOILER FOR $CO_2$ CAPTURING (순산소 재순환 연소를 채택한 $CO_2$ 회수형 보일러 연소실에 대한 수치해석)

  • Ahn, J.;Kim, H.J.
    • 한국전산유체공학회:학술대회논문집
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    • 2009.04a
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    • pp.329-334
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    • 2009
  • An oxy-fuel boiler has been developed to capture $CO_2$ from the exhaust gas. FGR (flue gas recirculation) is adopted to be compliant with the retrofit scenario. Numerical simulations have been performed to study the detailed physics inside the combustion chamber of the boiler. The temperature field obtained from the simulation agrees with the flame image from the experiment. The FGR combustion yields similar heat transfer characteristics with the conventional air combustion while the flame is formed further downstream in case of the FGR combustion.

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Effects of Fuel-Air Unmixedness on Lean Premixed Combustion Characteristics (연료-공기 비혼합도가 희박예혼합 연소 특성에 미치는 영향)

  • Kim, Dae-Hyun;Lee, Jong-Ho;Jeon, Chung-Hwan;Chang, Young-June
    • 한국연소학회:학술대회논문집
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    • 2002.06a
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    • pp.133-139
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    • 2002
  • The lean premixed technique has been proven very efficient in reducing NOx emissions from gas turbine combustors. However combustion instability is susceptible to occur in lean premixed combustor. So laboratory-scale dump combustor was used to understanding the underlying mechanisms causing combustion instabilities. In this study, tests were conducted at atmospheric pressure and inlet air was up to $360^{\circ}C$ with natural gas. The observed instability was a longitudinal mode with a frequency of ${\sim}341.8Hz$. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various equivalence ratio. Combustion instability was observed to occur at higher value of equivalence ratio(>0.69). This study was performed to investigate the effects of equivalence ratio and fuel split measuring NOx and acoustic wave. The results reveal the effect of fuel-air unmixedness on lean premixed combustor.

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Combustion Emission Characteristics on the Effect of Secondary Air Injection in Model Gas Turbine Combustor (모형 가스터빈 연소기의 2차공기 주입에 따른 연소배출특성)

  • 김규성;임경달;이도형
    • Journal of Ocean Engineering and Technology
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    • v.14 no.3
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    • pp.84-89
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    • 2000
  • The purpose of this study is to investigate the combustion emission characteristics by the effect of secondary air injection and variation of the excess air ratio in combustion field of model gas turbine combustor. For this purpose, mean temperature, CO, $CO_2$, $O_2$ and HC concentrations were measured by changing excess air ratio and secondary air injection. As a result of this study, mean temperature was decreased and CO, HC emission increased by increasing the excess air ratio of secondary air. Therefore, this results showed the secondary air injection effected strongly on the flame structure and combustion emission characteristics.

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Analysis on Combustion Characteristics of the Oil Burner using Swirl Flow (스월 유동을 이용한 오일 버너의 연소성능분석)

  • Choi, Chang-Woo;Kim, Young-Hwan;Jeong, Jae-Hyun;Park, Kweon-Ha
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2005.06a
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    • pp.1-8
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    • 2005
  • This paper addresses the analysis of the combustion characteristics in the oil burner using swirl flow. The reduction of exhaust emissions and high efficiency combustion techniques of the industrial burner have been studied to conserve environmental resources. We make swirl burner equal to dimension of wide burner and it is turn round of the combustion gas in construction. For a vigorous inner flow possessde 3m/s velocity in combustion gas of two burners. In calculation, we make use of a densely mesh to detailed analysis. In this study, the effect of swirl flow on the combustion of a commercial burner is analysed by experimental and also simulative manner. The results show the swirl burner has 40% better efficiency and less emissions of CO, HC, NOx and Smoke.

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Analysis of the Characteristics of Flue Gas in Infrared Mobile Heaters for Gas Room Heating (가스난방용 적외선 히터의 연소배기가스 특성해석)

  • Kim Young-Gyu;Kwon Jeong-Rock;Kim Chung-Kyun
    • Journal of the Korean Institute of Gas
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    • v.2 no.1
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    • pp.66-73
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    • 1998
  • This paper deals with the combustion characteristics of flue gas in infared mobile heaters. The experimental work has been performed to obtain the concentration levels and combustion characteristics of flue gas with varying chamber size and room temperature. The experimental results showed that oxygen depletion sensor device was operated at the oxygen concentration level of $18.3\%$ for all the chamber size. The combustion characteristics of oxygen and carbon dioxide show a linearity After 10 minutes the combustion property of carbon monoxide occurs at random without a level of oxygen and carbon dioxide in closed space of the heater. In these results, it is very important to prevent incomplete combustion through a sufficient ventilation, and accident prevention with a reduction of the oxygen and diffusion of toxic carbon monoxide.

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Study on the Ignition Characteristics of Liquid Rocket Engine Combustor and Gas Generator (액체로켓엔진 연소기 및 가스발생기의 점화 특성 연구)

  • Kim, Seung-Han;Moon, Il-Yoon;Lee, Kwang-Jin;Kim, Jong-Kyu;Seo, Seong-Hyun;Kim, Seong-Ku;Seol, Woo-Seok
    • 한국연소학회:학술대회논문집
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    • 2003.12a
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    • pp.139-143
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    • 2003
  • Study on the ignition characteristics of combustor and gas generator for LOx-kerosene liquid rocket engine was performed experimentally through a series of combustion tests of sub-scale engine combustor and gas generator. Characteristic of gas-torch ignitor based on gaseous methane and gaseous oxygen was compared with hypergolic ignition using propellant tri-ethyl-aluminium. Gas-torch ignitor showed good performance on igniting sub-scale liquid rocket engine combustor and gas generator. It was observed that the ignition delay is also affected by the extent of nitrogen in the combustion chamber.

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