• Title/Summary/Keyword: 추가연소기

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A Study on the Combustion Test of Artificial Turf Installed on Field (실외에 설치되는 인조잔디의 연소시험에 관한 연구)

  • Min, Se-Hong;Kim, Yeon-Hwang
    • Fire Science and Engineering
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    • v.28 no.2
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    • pp.48-53
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    • 2014
  • In this study, we would evaluate fire risk by domestic standard for artificial turf installed on field and roofs. Today domestic regulation for artificial turf only applies to outdoor uses and especially KS M 3888-1 has compulsion but limited to school athletic facilities. Indoor regulation complying with National Emergency Management Agency (No. 2012-35) was enacted as recommendations. Thus this study did combustion test of artificial turf installed on field. Analyzed result by 45 degree flammability test, standard was inadequate to judge the fire risk so we compared and analysed its characteristic through combustion test of flame retardant finishing carpet used as flooring. Test and assessment result of its ignitionability by 45 degree flammability test showed that carpet was satisfied with flame retardant finishing performance standard contrary to artificial turf. For this reason, by conducting cone calorimeter test, the combustion property after ignition would be analyzed and evaluated and then this study will suggest a countermeasure for strengthening standard.

Cooling Performance Analysis of Regeneratively Cooled Combustion Chamber (재생냉각 연소실의 냉각성능 해석)

  • Cho, Won-Kook;Seol, Woo-Seok;Cho, Gwang-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.4
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    • pp.67-72
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    • 2004
  • A regenerative cooling system has been designed through empirical 1-D analysis for a liquid rocket engine of 30-ton-level thrust. The hot-gas-side wall temperature from 1-D analysis shows 100K difference compared to 3D CFD analysis. Two variations of design with same cooling performance are suggested for different maximum channel widths i.e., 4mm and 2mm. The coolant pressure drop of the latter design is higher by 20%. The maximum liner temperature is about 700K when TBC and the thermal resistance of carbon deposit are considered. So film cooling is recommended to increase the cooling capacity as the present cooling capacity is insufficient

Numerical Simulation on Particle Dispersion in Axisymmetric Sudden-Expansion by Tracer Method (입자추적법에 의한 축대칭 급확대부의 입자확산현상 수치해석)

  • Park, Ounyoung;Yang, Hee Sung;Yim, Chung Sik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.766-774
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    • 2017
  • Software has been developed for simulating particle dispersion in a circular pipe with sudden-expansion, which models the fuel feeding system of a combustor that uses metal powder like aluminum as fuel. The Lagrangian based discrete tracer point method was employed for a plug flow of particles that satisfies local turbulent velocity fluctuations. A radial velocity component was created to improve the flow turning outwards in the recirculation zone. The particle distribution patterns from both with and without the component were directly compared with the experiments near the reattachment.

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A Fundamental Study of Hybrid Combustion System Applying Exhaust Gas Recirculation (배기가스 재순환을 적용한 하이브리드 연소시스템에 대한 기초 연구)

  • Oh, Wheesung;Yu, Byeonghun;Park, Taejoon;Lee, Chang-Eon
    • Journal of Energy Engineering
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    • v.25 no.1
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    • pp.100-107
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    • 2016
  • In this study confirmed the reduction effect of pollutant by applying Fi-EGR and FPI-EGR to hybrid combustion system realizing premixed flame and non-premxied flame at once. The results showed that NOx emission index decreased significantly in case of adopting EGR. Additionally, the hybrid combustion system with EGR resulted in a better performance compared to usual non-premixed combustion system such that it can reduce $NO_x$ emission at equivalent EGR ratios. Especially, in the case of 25% of FI-EGR ratio at hybrid combustion system that the ratio of non-premixed and premixed is 50 : 50, NOx emission index reduction rate was about 59% compared to $NO_x$ emission of non-premixed combustion system without EGR and in the case of 15% of FPI-EGR ratio at hybrid combustion system that the ratio of non-premixed and premixed is 70 : 30, $NO_x$ emission index reduction rate was about 48% compared to $NO_x$ emission of hybrid combustion system without EGR.

Performance Analysis of Methane Fueled Marine Solid Oxide Fuel Cell and Steam Turbine Hybrid Power System (선박동력용 SOFC/ST 하이브리드시스템의 성능 평가)

  • Lee, Kyung-Jin;Oh, Jin-Suk;Kim, Sun-Hee;Oh, Sae-Gin;Lim, Tae-Woo;Kim, Jong-Su;Park, Sang-Kyun;Kim, Mann-Eung;Kim, Myoung-Hwan
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.5
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    • pp.590-599
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    • 2011
  • The electrification of the waste heat of fuel cell is necessary to enhance the efficiency of fuel cell system. For this purpose, the SOFC/ST(Solid oxide fuel cell/Steam turbine) hybrid system is suitable. The purpose of this work is to predict the performance of methane fueled SOFC/ST hybrid power system and to analyze the influence of operating temperature of stack, current density of stack, combustor outlet gas temperature, and boiler outlet gas temperature. According to the analysis, it is proved that making the best use of the waste heat of stack and minimizing the fuel consumption of combustor are essential for the high-efficiency of SOFC/ST hybrid system.

Improvement of Post-combustion CO2 Capture Process using Mechanical Vapor Recompression (기기적 증기 재압축 시스템을 적용한 연소 후 이산화탄소 포집공정 개선 연구)

  • Jeong, Yeong Su;Jung, Jaeheum;Han, Chonghun
    • Journal of the Korean Institute of Gas
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    • v.20 no.1
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    • pp.1-6
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    • 2016
  • In order to reduce the anthropogenic emission of greenhouse gases, CCS technology has emerged as the most promising and practical solution. Among CCS technology, post-combustion $CO_2$ capture is known as the most mature and effective process to remove $CO_2$ from power plant, but its energy consumption for chemical solvent regeneration still remains as an obstacle for commercialization. In this study, a process alternative integrating $CO_2$ capture with compression process is proposed which not only reduces the amount of thermal energy required for solvent regeneration but also produces $CO_2$ at an elevated pressure.

Investigation of Tar/soot Yield of Bituminous and Low Rank Coal Blends (발전용 역청탄과 저열량탄 혼소시 Tar/Soot의 배출 특성 연구)

  • Lee, Byung Hwa;Kim, Jin Ho;Kim, Gyu Bo;Kim, Seng Mo;Jeon, Chung Hwan
    • Journal of Energy Engineering
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    • v.23 no.2
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    • pp.42-48
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    • 2014
  • Soot and tar which were derived from combustion or pyrolysis processes in Puverized Coal(PC) furnace or boiler have been significantly dealing in a radiative heat transfer and an additional source of NOx. Furthermore, the increasing for the use of a coal with low caloric value gives rise to a lot of tar-soot yield and LOI in a recycled ash for using cement materials. So, the ash with higher tar-soot yield and LOI can not recycle due to decreased strength of concrete. In this study, tar-soot yields and flame structures were investigated using the LFR for a blending combustion with bituminous coal and sub-bituminous coal. Also, The investigation were conducted as each single coals and blending ratio. The coals are used in a doestic power plant. In the experimental results, sub-bituminous coal with high volatile contents shows longer soot cloud length than bituminous coal, but overall flame length was shorter than bituminous coal. Tar-soot yields of sub-bituminous coal is lower than those of bituminous coal. Combustion characteristics are different between single coal and blended coal. Therefore, finding an optimal coal blending ratio according to coal rank effects on tar-soot yields.

Study of Cooling Performance Enhancement on Injector Face Plate of Rocket Engine (로켓엔진 분사면의 냉각성능 향상에 관한 연구)

  • Cho Won Kook;Seol Woo Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.215-218
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    • 2005
  • An optimal fuel manifold is suggested to improve the cooling performance of injector face plate. The cooling performance at the center area of the injector face plate is to be augmented while the spatial injection uniformity is maintained. The comparison of the cooling performance of 7 candidates gives the conclusion that the dividing plate from 2-3 injector row to 9-10 injector row is an optimal. The maximum face plate temperature decreases by $27\%$ while the injection uniformity is close to that of the original design. The pressure drop in the fuel manifold of the optimal design is also same as the original design.

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A Theoretical Performance Analysis of Small Liquid Rocket Engine for Space Vehicle Attitude Control (우주비행체 자세제어용 소형 액체로켓엔진의 이론성능 해석)

  • Kim Jeong-Soo;Park Jeong;Kim Sung-Cho;Choi Jong-Wook;Jang Ki-Won
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.196-200
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    • 2005
  • A theoretical model for the calculation of chemical equilibrium composition of propellant combustion product is briefly presented for the performance analysis of monopropellant hydrazine rocket engine. Analysis result is compared to that of test and evaluation of 1-lbf class thruster and is scrutinized primarily from the view point of ammonia dissociation fraction. Chemical equilibrium composition and average molecular weight is additionally depicted according to the variation of propellant inlet pressures and the varying nozzle area ratio. The theoretical analysis is tried as a way of derivation of design parameters for mid- and large-thrust class of monopropellant rocket engines.

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Cooling Performance Enhancement of a Rocket Engine Injector Face Plate (로켓엔진 분사면의 냉각성능 향상)

  • Cho Won Kook;Seol Woo Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.3
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    • pp.92-100
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    • 2005
  • An optimal fuel manifold is suggested to improve the cooling performance of an injector face plate. The cooling performance at the center area of the injector face plate is to be augmented while the spatial injection uniformity is maintained. The comparison of the cooling performance of f candidates gives the conclusion that the dividing plate from 2-3 injector .ow to 9-10 injector. row is an optimal. The maximum face plate temperature decreases by 27$\%$ while the injection uniformity is close to that of the original design. The pressure drop in the fuel manifold of the optimal design is also same as the original design.