• Resources Recycling
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• v.9 no.6
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• pp.15-22
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• 2000

There are many intensive efforts to develop the recycling technologies of waste plastics in steel works to tackle the saving of resources and the protection of the natural environment. In this study, the thermogravimetric analyses for three kinds of plastics, the combustion experiments and the theoretical approach for calculating the flame temperature in the blast furnace had been performed to understand the behavior of plastics in the raceway. The thermal decompositions of plastics were studied using thermogravimetric analyzer under the atmospheric condition. The starting temperature of thermal decomposition and the maximum weight loss point were increased in proportion to the logarithmic values of heating rate. The combustion characteristics of plastics were simulated in a coke-bed combustor. The combustion efficiency of plastics was lower than that of pulverized coal. The oxygen enrichment was found out to be one of the useful methods to increase the combustibility of plastics in raceway. The maximum injection rate of plastics was calculated based on the flame temperature.

• Resources Recycling
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• v.23 no.6
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• pp.47-53
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• 2014

Effective treatment and energy conversion technologies are necessary due to the ban of the dumping of organic waste including the sewage sludge. In this study, the kinetics of pyrolysis and combustion were derived in a TGA and thermobalance reactor, which is essential for thermal conversion of sewage sludge to energy. Three steps are shown for the pyrolysis in TGA and the different pre-exponential factors and activation energies are derived depending on the temperature range. Three models of gassolid reaction were applied to the reaction kinetics analysis for the combustion of sewage sludge char and shrinking core model was an appropriated model. Apparent activation energy and pre-exponential factor were evaluated and the effect of oxygen partial pressure was examined.

• Journal of the Korean Society of Propulsion Engineers
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• v.2 no.3
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• pp.54-61
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• 1998

A numerical simulation is attempted for the regenerative cooling heat transfer processes of the liquid propellant rocket engine. The heat transfer from the combustion gases to the thrust chamber wall is called gas side heat transfer. This heat is conducted radially to the coolant through the carbon deposit and metallic wall of thrust chamber Finally, this heat is convected away by the coolant flowing along the passages in the thrust chamber. The equivalence of these three heat fluxes of the above processes is utilized to determine the coolant side wall temperature, gas side wall temperature and the heat flux. When the number and shape(width, height) of coolant passages, the shape(size) of thrust chamber, oxidant and fuel properties, coolant properties, oxidant/fuel mixture ratio, coolant inlet temperature, the thickness of carbon deposit formed along the thrust chamber wall during combustion are given, reasonable radial direction temperature distributions and heat fluxes along the thrust chamber axis are obtained.

• Fire Science and Engineering
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• v.33 no.3
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• pp.29-36
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• 2019

The combustion properties required for fire simulations of multi-layer, multi-component flame retardant cables were measured using a cone calorimeter. The CO and soot yields combustion efficiencies of the flame retardant cables were investigated. TFR-8 (flame retardant PCV and XLPE added), TFR-CVV-SB (flame retardant PCV and general PVC), and VCTF, which are excellent in the flame retardancy of cables, were considered. As the main result, the CO yield (y_CO) of the TFR-8 and TFR-CVV-SB flame retardant cables increased by 23% and 16%, respectively, with increasing incident radiation heat flux from 25 kW/㎡ to 50 kW/㎡. On the other hand, the CO yield of VCTF was not influenced significantly by the changes in radiant heat flux. Finally, the soot yield and combustion efficiency increased as the sheath material (flame retardant performance) was strengthened. Therefore, in a fire environment where various heat fluxes coexist, attention should be paid to the top of the application of the combustion property of the flame retardant cable.

• 한국신재생에너지학회:학술대회논문집
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• 2010.11a
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• pp.81.2-81.2
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• 2010

고체 산화물 연료전지(SOFC) 시스템은 스택과 기계적 주변 장치인 MBOP(Mechanical Balance of Plant), 그리고 전기적 주변장치인 EBOP(Electrical Balance of Plant)로 구성되어있다. SOFC는 일반적으로 $700^{\circ}C$ 이상의 고온에서 작동되기 때문에 효율적인 열 이용 및 열 관리가 중요하다. SOFC 시스템의 MBOP에는 상온의 연료가스들을 고온으로 가열하여 스택에 유입 시기키 위한 열교환기 및 촉매연소기 등의 장치들이 필요하며, 효율적인 열관리를 위해서는 고온에서 작동하는 장치들을 한곳에 통합하여 구성하는 것이 필수적이다. 본 연구에서는 SOFC 시스템의 MBOP(Mechanical Balance of Pant) 중 고온부에 해당하는 촉매연소기, 열교환기 및 스택이 통합된 스택 모듈을 제작에 앞서 개념 검증을 위해 열교환기 및 촉매연소기로 이루어진 프로토타입(prototype)의 SOFC 모듈평가 장치를 제작하였다. 열교환기는 Plate형으로 총 6개로 구성되어 있으며, 연료극과 공기극 가스라인에 각각 3개씩 배치하여 스택에 유입되는 연료 및 공기가 촉매연소기에서 나오는 고온의 배가스와 열교환되어 가열되도록 구성하였다. 촉매연소기는 honeycomb 타입의 촉매를 사용하였고, 촉매연소기로 유입되는 연료극 배가스와 공기의 균일혼합과 hot spot을 방지하기 위한 장치를 삽입하여 제작하였다. 제작된 SOFC 모듈평가장치는 시운전을 통해 각 장치의 성능 확인 후 반응면적이 $20{\times}20cm^2$ 인 단전지를 적층하여 연계 운전을 수행하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2002.04a
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• pp.2-3
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• 2002

일반적으로 연소과정에서 발생한 고온고압의 연소가스로 인하여 액체추진기관의 연소실 및 노즐 벽면 그리고 추진기관 후방부위에 대류열전달(Convective heat transfer)과 복사열전달(Thermal radiative heat transfer)이 발생하는 것으로 알려져 있으며, 액체추진기관에서 발생하는 복사열전달 현상은 재생냉각장치의 열입력량 예측 및 발사체의 추진기관 후방부위에 탑재되는 전자장이 및 구조물의 열적환경(Thermal environmental phenomena)을 분석하는데 매우 중요하다. 이에 본 연구에서는 노즐 후방부위에서 발생하는 복사열전달량(Radiative heat transfer rate)을 측정하고 연소압(Chamber pressure)과 혼합비(Mixture ratio)에 따른 영향을 파악하였다.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1993.11a
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• pp.88-91
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• 1993

유동층 반응기 (H=0.8 m, ID=0.08 m) 에서 폐타이어의 열분해를 수행함에 있어 열분해에 사용되는 열을 외부에서 공급함과 동시에 일부는 내부에서 자체적으로 연소시켜 열을 얻고자 하였다. 온도 증가에 따라 가스의 수율은 40 %까지 증가하였고, 반면에 오일의 수율은 감소하였다. 또한 가스중에 heavy hydrocarbon 이 감소함과 동시에 H$_2$ 및 light hydrocarbon 이 증가하였고 이로 인해 가스 부피당 발열량은 감소하는 것으로 나타났다. 가스의 체류시간도 가스조성에 상당히 영향을 미치는 것으로 나타났으며, 본 시스템에서 발열량 및 가스생성량은 2 u$_{mf}$ 에서 최소치를 나타내는 것으로 보였다. 또한 $O_2$ 농도의 증가는 결국에는 생성가스의 연소를 일으키며, 적당한 $O_2$ 농도의 설정으로 이의 연소를 최소화하는 작업이 필요하다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.406-407
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• 2009

The thermal protection techniques for ramjet combustor are key technology, which block the heat from hot combustion gas, and maintain the structure temperature safely. Film cooling method is one of them. This research proposes the optimal thermal design method through performing the study of thermal protection design for ramjet combustor.

• Journal of Energy Engineering
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• v.17 no.2
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• pp.100-106
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• 2008

Flameless fiber mat catalytic burners have been known as an effective heat source in industrial drying processes since heat obtained from combustion can be transferred to absorptive body by far-infrared radiation. In order to extend the application of fiber mat catalytic burner, novel fiber mat catalytic burners were manufactured and combustion characteristics of them were investigated. For diffusive catalytic burners, the efficiency of combustion was significantly affected by the installation direction and the temperature of catalytic bed perimeter influenced on the diffusion rate of oxygen which determined the combustion efficiency of catalytic burner. It was seen in premixed catalytic combustion that air content in premixed fuel gas was optimized at slightly higher than theoretical amount of air. Combustion heat released higher than 70% by radiant heat in premixed catalytic combustion likewise diffusive catalytic combustion.

• Journal of Energy Engineering
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• v.13 no.2
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• pp.112-117
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• 2004

Volatile organic compounds (VOCs) are low calorific value gases (LCVG) emitted from chemical processes such as painting booth, dye works and drying processes etc. Characteristics of VOCs are low calorific values less than 150kcal/㎥, high activation energy for ignition and low energy output. These characteristics usually make combustion unstable and its treatment processes needs high-energy consumption. The cyclone combustion system is suitable for LCVG burning because it can recirculate energy through a high swirling flow to supply the activation energy for ignition, increases energy density In make a combustion temperature higher than usual swirl combustor and also increases mixing intensity. This research was conducted to develop optimized cyclone combustion system for thermal oxidation of VOCs. This research was executed to establish the effect of swirl number with respect to the combustion temperature and composition of exhausted gas in the specific combustor design.