• Title/Summary/Keyword: 혼합 산화제

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The Effect of Focal Length on Fuel Mixing And Combustion in One-focusing Oxygen Burner (일 초점 산소 버너의 초점 거리가 연료 혼합 및 연소에 미치는 영향)

  • Park, Kweon-Ha;Kim, Ju-Youn
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.6
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    • pp.814-819
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    • 2011
  • An Oxy-fuel combustion has been studied in order to reduce exhaust emissions and fuel consumption. The flow and flame behaviors are analyzed with focal length variation in one-focussing oxygen burner introduced in this study. Oxygen is supplied into the center of the nozzle, methane fuel is into the outer nozzle of the center, and then oxygen is again supplied into the outer of the fuel nozzle. The test conditions are 5 focal lengths of 100mm to 500mm. The mixing behaviors and temperature distributions are analyzed. The result shows that the shorter the focal length is, the longer the mixing length becomes, and the flame width and length are the biggest in the case of 300mm.

Comparison of Fuel-NOx Formation Characteristics in Conventional Air and Oxyfuel Combustion Conditions (일반 공기 및 순산소 연소 조건에서 Fuel-NOx 생성 특성의 비교)

  • Woo, Mino;Park, Kweon Ha;Choi, Byung Chul
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.5
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    • pp.481-488
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    • 2013
  • Nitric oxide ($NO_x$) formation characteristics in non-premixed diffusion flames of methane fuels have been investigated experimentally and numerically by adding 10% ammonia to the fuel stream, according to the variation of the oxygen ratio in the oxidizer with oxygen/carbon dioxide and oxygen/nitrogen mixtures. In an experiment of coflow jet flames, in the case of an oxidizer with oxygen/carbon dioxide, the $NO_x$ emission increased slightly as the oxygen ratio increased. On the other hand, in case of an oxygen/nitrogen oxidizer, the $NO_x$ emission was the maximum at an oxygen ratio of 0.7, and it exhibited non-monotonic behavior according to the oxygen ratio. Consequently, the $NO_x$ emission in the condition of oxyfuel combustion was overestimated as compared to that in the condition of conventional air combustion. To elucidate the characteristics of $NO_x$ formation for various oxidizer compositions, 1D and 2D numerical simulations have been conducted by adopting one kinetic mechanism. The result of 2D simulation for an oxidizer with oxygen/nitrogen well predicted the trend of experimentally measured $NO_x$ emissions.

Fire Hazard of PP and LLDPE dust in Chemical Plant Process (석유화학플랜트에서 발생하는 PP(Poly Propylene) 및 LLDPE(Linear Low Density Poly Ethylene) 분진의 연소 위험성에 관한 연구)

  • 김정환;이창우;현성호;권경옥
    • Fire Science and Engineering
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    • v.15 no.1
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    • pp.16-22
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    • 2001
  • Thermal properties of PP and LLDPE dusts from chemical plant and their risks of coexisting with oxidizer were investigated by a pressure vessel. The thermal decomposition of PP and LLDPE dusts with temperature using DSC and the weight loss with temperature using TGA were also investigated to find the thermal hazard of PP and LLDPE dusts. Using the pressure vessel which can estimate ignition and explosion of PP and LLDPE dusts coexisting with oxidizer, a series of bursting of a rupture disc, experiments has been conducted by varying the orifice diameters the weight ratio of the sample coexisting with oxidizers and the species of oxidizer. And fire gases was measured by gas analyser ($ECOM-A^+$). According to the results of the thermal analysis of PP and LLDPE dusts, the decomposition temperature range of PP and LLDPE dusts was 200 to 350 and 300 to $500^{\circ}c$, respectively. The risk of PP and LLDPE dusts coexisting with oxidizer was increased as the orifice diameter was decreased. On the other hand, it was increased as the weight ratio of the sample to the oxidizer were increased. In addition, the risk of PP and LLDPE dusts coexisting with oxidizer was affected by the decomposition temperature of the sample and oxidizer. It is found that the risk of fire becomes high when the decomposition temperature of the sample is about same as that of oxidizer. Also, the fire gases was occurred carbon monoxide and carbon dioxide. The amount of carbon monoxide generated was found to be much higher in PP decomposition than in LLDPE due to incomplete combustion of PP which has high content of carbon in chemical compound.

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Flame Instability in Heptane Pool Fires Near Extinction (소화근처 헵탄 풀화재의 화염불안정성)

  • Jeong, Tae Hee;Lee, Eui Ju
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.12
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    • pp.1193-1199
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    • 2012
  • A cup burner experiment was performed to investigate the effect of the oxidizer velocity and concentration on flame instability near extinction. Heptane was used as a fuel and air diluted by nitrogen and carbon dioxide was used in the oxidizer stream. Two types of flame instabilities at the flame base and at axial downstream were observed near extinction. The instability at the flame base could be characterized by cell, swing, and rotation modes, and the cell mode changed to the rotation mode through the swing mode as the oxidizer velocity increased. To assess the parameters for the flame instability, the initial mixture strengths, Lewis number, and adiabatic flame temperature were investigated under each condition. The Lewis number might be the most important among them, but it is impossible to generalize because of the insufficient number of cases. Furthermore, the axial periodic flickering motion disappeared at low and high oxidizer velocities near extinction. This resulted from the fact that low oxidizer velocity induced evaporated fuel velocity below the critical velocity and high velocity made the reacting fuel velocity comparable.

매립장 침출수에 의한 오염지하수 정화 방법 연구

  • 송나인;도원홍;이민희
    • Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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    • 2004.04a
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    • pp.413-416
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    • 2004
  • 매립장 침출수로 인해 오염된 매립장 주변 지하수 정화를 위한 실내실험을 실시하였다. 오염물로는 대표적 염화용제인 TCE와 PCE, 그리고 중금속인 As, Cd, Cr, Pb에 대하여 Air-sparging, 오존 산화법, 화학적 처리방법에 의한 정화효율 실험을 실시하였다. Air-sparging은 TCE, PCE에서 높은 제거효율을 가졌으며, 오존 산화법은 Cr, Pb에서 제거 효율이 좋았다. 반응제를 첨가한 공침방법의 경우, 모든 중금속에 대하여 소석회 첨가시 매우 높은 제거효율을 보였으며, As는 황산제일철에서, Cd, Cr, Pb는 탄산칼슘과 제올라이트 첨가시 높은 제거효율을 나타내었다. 실험결과로부터, 유기오염물과 중금속이 혼합되어 나타나는 매립장 주변 오염 지하수의 경우 휘발성 유기오염물의 제거를 위해서는 폭기방법이, 중금속의 경우에는 공침방법에 의해 수산화물, 탄산염으로 만들어 고형물로 처리하는 방법이 제거효과가 좋은 것으로 나타났다.

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Development of Porous Sorbents for Removal of Hydrogen Sulfide from Hot Coal Gas -I. Additive Effect of Sorbents for the Removal of Hydrogen Sulfide- (고온석탄 가스에서 황화물의 제거하기 위한 다공성 흡착제의 개발-1. 황화수소가스 흡착제의 첨가물 효과-)

  • 이재복;류경옥
    • Journal of Environmental Health Sciences
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    • v.14 no.1
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    • pp.1-9
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    • 1988
  • 석탄유도가스에 포함된 황화수소를 제거시킬 흡착제를 개발하기 위하여 알칼리 토금속, 천이원소 및 아연의 이온반경보다 이온반경이 작은 금속산화물을 산화아연에 첨가시켜 다공성 흡착제를 제조하였다. 600$\circ$C에서 이들 첨가시료를 2.09vol.% 황화수소와 질소가스 혼합기체로 반응시켜 초기속도를 측정하고, 같은 온도에서 사용된 흡착제를 공기로 재생시켰다. 사용된 금속산화물 첨가 흡착제중에서 CaO, TiO$_2$, $Fe_2O_3$, CuO, $Ga_2O_3$ 및 Si$_2$O가 ZnO 흡착제의 초기속도를 증가시켜 첨가제로 사용할 수 있음을 보였다.

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자속의 피닝과 열적 크리프

  • Gang, Gwang-Yong;Seo, Jeong-Dae;Lee, Jong-Yong;Seong, Geon-Yong
    • Electronics and Telecommunications Trends
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    • v.6 no.3
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    • pp.66-76
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    • 1991
  • 산화물 고온초전도체는 제2종 초전도체 이므로 초전도 혼합상태에 대한 해석과 고온초전도 메카니즘의 규명과는 직접적으로 관련되어 있다. 특히 자장하에서 생겨나는 여러가지 물성이 산화물 초전도체의 구조 및 메카니즘 연구에 밝은 전망을 던져 주므로 이론 및 실험과학자들에게 큰 관심을 불러 일으키고 있다. 한편, 산화물 고온초전도체는 $T_c$가 높기 때문에 noise를 포함한 열적 특성이 저온초전도체와 사뭇 다르며 고자장하의 $T_c$근처에서, 전류-전압특성등의 물성에 비선형성(nonlinearty)이 많이 나타난다. 이러한 특성과 관련하여 고온초전도체의 한면을 설명하고자 한다.

Toxicity Reduction of VOCs by Catalytic Oxidation Mechanism (VOCs의 촉매산화 메커니즘에 의한 독성 저감효과)

  • 이재동
    • Journal of environmental and Sanitary engineering
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    • v.15 no.3
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    • pp.88-93
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    • 2000
  • The objective of this study was to depict the kinetic behavior of the platinum catalyst for the deep oxidation of VOCs and their mixture. The oxidation characteristics of VOCs, which were benzene, toluene, and styrene, was studies on a 0.5% $Pt/{\gamma}-Al_2O_3$ catalyst. The reactivity increases in order benzene>toluene>styrene. In mixtures, remarkable effects on reaction rate and selectivity have been evident ; the strongest inhibiting effect was shown by styrene and increases in a reverse order with respect to that of reactivity. The reaction model reveals that there is a competition between the two reactants for the oxidized catalyst. Thus, the nontoxic catalytic oxidation process was suggested as the new VOCs control technology.

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Formation Mechanism of Chlorate ($ClO_3\;^-$) by Electrochemical Process (전기화학적 공정에 의한 클로레이트의 생성메커니즘)

  • Baek, Ko-Woon;Jung, Yeon-Jung;Kang, Joon-Wun;Oh, Byung-Soo
    • Journal of Korean Society of Environmental Engineers
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    • v.31 no.8
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    • pp.627-634
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    • 2009
  • This study was done to find out the formation mechanism of chlorate by electrochemical process using chloride ion ($Cl^-$) as an electrolyte. Firstly, the effective factors such as pH and initial chloride concentration were figured out to see the formation property of chlorate during electrolysis. And the relation of free chlorine, and mixed oxidants such as OH radical and ozone with chlorate were estimated to concretize the formation mechanism. As a result, it was found that the major reaction of chlorate formation would be electrochemical reaction with free chlorine, and also the direct oxidation of chloride ion and the reaction by OH radical were participated in the formation of chlorate. Moreover, it was observed that formed chlorate was oxidized to perchlorate. Lastly, the optimum condition was recommended by comparing free chlorine with chlorate concentration during the electrochemical process with the different electrode separation.

Effect of Propellant-Supply Pressure on Liquid Rocket Engine Performance (추진제 공급압력이 액체로켓엔진의 성능에 미치는 영향)

  • Cho, Won-Kook;Park, Soon-Young;Nam, Chang-Ho;Kim, Chul-Woong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.4
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    • pp.443-448
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    • 2010
  • In this paper, the changes in performance parameters, e.g., the combustor pressure, turbine power, engine mixture ratio, temperature of gas generator, and product gas, of a liquid rocket engine employing gas generator cycle with the variations in propellant-supply pressure have been described. Engine performance is numerically calculated using the 13 major system-level variables of the rocket engine. The combustor pressure and turbine power increase with an increase in the oxidizer-supply pressure and decrease with an increase in fuel-supply pressure. The lower mixture ratio of gas generator for increased fuel mass flow rate decreases the gas generator gas temperature and deteriorates the gas material properties as the turbine working fluid. The turbine power decreases with an increase in fuel-supply pressure; this results in a decrease in the main-combustor pressure, which is directly proportional to engine thrust.