• Resources Recycling
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• v.15 no.1 s.69
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• pp.46-57
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• 2006

For the development of combustion technology of RDF(refuse derived fuel), combustion characteristics are examined in bubbling fluidized bed, circulating fluidized bed, continuos combustor and batch type combustor. The characteristics of combustion and exhaust gas has been compared and analyzed in many type of combustion facilities, which has been utilized as basic data for the advanced research of specified RDF combustion facility. Stable combustion has been observed in bubbling and circulating fluidized bed from controled operating condition like the proper feeding rate and superficial gas velocity. In circulating fluidized bed, concentration of NOx has been increased with the operating condition by the fuel-NO and oxygen reaction and $SO_2$ can be considered not to be produced in RDF fluidized bed from very low concentration in flue gas. HCl concentration is 36.4 ppm as average value and lower than standard emission value, but the counter plan is needed. Shaped RDF and fluff RDF have been compared in continuos combustor and batch type combustor and shaped RDF shows benefit for the stable heat recovery and gas emission shows similar value and characteristics.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.2
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• pp.92-97
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• 2005

A series of combustion test was done to verify the optimization result of a gas generator for a 10 ton thrust liquid rocket engine. An injector element is F-O-F impinging type injector and the test was conducted with kerosene/LOX propellants. Test results of combustion temperature and pressure show a very good agreement with optimal design result and verify that the design method was properly established. And turbulence ring revealed its effectiveness in enhancing combustion gas mixing and temperature difference in the radial direction showed only less than 15K. Also turbulence ring induced only 3.2% pressure loss in the combustion chamber, which is far less than conventional level observed in a gas turbine engine. Axial temperature distribution also shows that turbulence ring could effectively reduce about 10% or more in gas generator length if its location is properly selected.

• Journal of Energy Engineering
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• v.23 no.3
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• pp.51-57
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• 2014

A MILD(Moderate and Intense Low oxygen Dilution) combustion, which is effective in the reduction of NOx, is considerably affected by the recirculation flow position of hot exhaust gas to the combustion furnace. A numerical analysis was accomplished to elucidate the flow characteristics in the MILD combustion incinerator for several cases with or without exhaust gas recirculation. It could be seen from the result of the present numerical study that the flow recirculation could be observed in the upper region over the vertical dividing wall for the case without exhaust gas recirculation. The optimal position of exhaust gas recirculation position was derived by the comparison of %RMS of x directional velocity for the cases with exhaust gas recirculation. The case with the exhaust gas recirculation position at the upper right of free board was the most effective with the smallest value of 57.4% RMS.

• Journal of the Korean Institute of Gas
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• v.19 no.6
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• pp.8-14
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• 2015

Synthetic natural gas(SNG), acquired from coal, is regarded as an alternative to natural gas since a rise in natural gas due to high oil price can be coped with it. In the present study, 11-liter heavy duty compressed natural gas(CNG) engine was employed in order to examine the combustion and emission characteristics of SNG. The simulated SNG, made up 90.95% of methane, 6.05% propane and 3% hydrogen was used in the experiment. Power output, thermal efficiency, combustion stability and emission characteristics were compared to those with CNG at the same engine operating conditions. Knocking phenomenon was also analyzed at 1260 rpm, full load condition. Combustion with SNG was more stable than CNG. Nitrogen oxides emissions increased while Carbon dioxides emissions decreased. Anti-knocking characteristics were improved with SNG.

• Proceedings of the Korean Institute of Industrial Safety Conference
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• 1998.11a
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• pp.109-113
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• 1998

압력조정기란 저장탱크와 용기로 부터 연소기에 공급되는 가스압력을 연소기의 압력에 맞게 조절하여 정상연소가 되도록 돕는 장치로써, 용기 및 저장탱크내의 압력변화에 대응하여 공급압력을 일정하게 유지하고, 가스의 조성, 온도, 소비량, 소비시간, 잔류가스량 등의 변화에 따라 감압작용과 정압작용을 동시에 하는 장치이다. LPG용 압력조정기는 일반가정용이나 업소에서 주로 사용하는 조정기로써 용량 4kg/h부터 집단공급용인 수백 키로까지의 제품이 있으며 일반적으로 감압작용, 정압작용, 폐쇄작용을 한다. (중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.225-228
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• 2009

Hot-firing tests were performed on the gas generator which is a technology development/demonstration model for a 75 ton-class liquid rocket engine. A heat-sink type combustion chamber was used for initial performance examination of the injector and mixing head. This paper explains not only preparation works for hot-firing tests but also the acquired results such as pressure, temperature distribution, and pressure fluctuation.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.05a
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• pp.266-269
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• 2003

During liquid rocket engine combustion, the resulting combustion gas has flow characteristics of high temperature and high velocity. An experimental study was performed to obtain basic data for a flame deflector design that is endurable under such flow characteristics. While the injected-water cools down the combustion plume, temperature and pressure of the plume was measured. As the experiment is being performed, gas temperature was measured using infrared cameras, and the gas temperature data was compared with the temperature data from the sensor in the plume. With the results of this experiment, we were able to obtain applicable temperature data for flame deflector design and predict the performance and structural strength required for installation of water injector.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.173-176
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• 2010

A subscale gas generator was designed and manufactured to understand a reason for increased pressure drop of liquid oxygen injectors observed in a technology demonstration model of a 75 ton-class gas generator. A total of 6 hot-firing tests were successfully performed including experimental conditions of design and off-design points. The hot-firing results showed that discharge coefficients of fuel and liquid oxygen remained constant as the mixture ratio varied at a fixed chamber pressure. At a fixed mixture ratio, it was also found that discharge coefficients of fuel and liquid oxygen was constant as the chamber pressure was increased.

• Journal of the Korean Institute of Gas
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• v.20 no.1
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• pp.46-51
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• 2016

This study is analyzed by the test equipment of gas analyzer in order to discover the gas characteristics of industrial plastic under the pyrolysis and combustion. As results, first, the pyrolysis of polycarbonate was started at $400{\sim}450^{\circ}C$. The combustion started at about $608^{\circ}C$, and the weight decreased at the velocity was 0.03g/min. Second, in case of polyethyleneterephtalate, PET was finished at $620^{\circ}C$ after starting pyrolysis from $420^{\circ}C$, and the weight decreased at the velocity of 0.044g/min. The pyrolysis velocity with the temperature of polyethyleneterephtalate rising was becoming slow and the pyrolysis temperature was higher with less added polyethyleneterephtalate.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.26 no.2
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• pp.192-203
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• 1990

여러 가지 다른 형태의 노즐을 공기 선회식 버너와 공기의 선회가 없는 버너(CB-125 Burner)에 장치하여 공기 분사식으로 오일을 분사하여 연소로에서 연소시켰다. 연소로는 길이 3m에 약 1m 상(3) 의 연소공간을 가졌으며 상부에는 열전대를 장치하고 하부에는 물이 흐르는 관을 설치하여 열효율을 계산할 수 있게 설계하였다. 연소로 연돌부에는 CO 하(2), CO, O 하(2) 가스 분석기를 사용하여 과잉공기량과 고온계로 배기가스 온도를 측정하도록 하였다. 모든 측정치는 연소곡선과 효율곡선에 의하여 얻어진 상수를 이용하여 계산한 연소로 성능방정식에 의하여 평가하였다. 실험치에 의해 계산한 벽면 열손실량과 열전달 공식에 의해 산출한 열손실량을 비교 분석하여 측정치의 정확도를 추정하고 과잉공기의 효과도 검토하였다. 그 결과 본 연구에서 사용된 두 종류의 버너와 여러 형태의 노즐이 오일 연소시 열효율 면에서 큰 차이를 보이지 않고 있음을 알았다.