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An Experimental Study on the Combustion Characteristics of Non Class 1E Cables 非1E类电缆燃烧特性的实验研究
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2019-03-31 DOI: 10.15231/JKSC.2019.24.1.015
H. Seo, Nam-Kyun Kim, Sang Kyu Lee, Y. Moon
The occurrence of a cable fire in a nuclear power plant can cause significant damage to the internal equipment and the defense system, and even reactor melt down in the worst case. In addition, toxic gases, released by burning cable jacket and insulation materials, can hinder human evacuation and fire fighting activities. Thus, this experimental study was conducted to investigate the toxicity of two non-class 1E cables which are applied to the nuclear power plants in Korea. Experiments were conducted for two kinds of cables according to the standard code of ISO 19702, and time series heat release rate, total heat release, and the concentration of toxic gases including CO, CO2, HCl, HCN, HBr, HF, NOx and SO2 were measured From the test results, the similar characteristics between heat release rate and CO2 emission and production of a small amount of halogenated compounds in emission gas caused by addition of fireproof components have been found. These results can be used as baseline data when assessing combustion characteristics and human toxicity of electric cables.
核电站电缆火灾一旦发生,会对内部设备和防御系统造成重大损害,最严重时甚至会导致反应堆熔毁。此外,燃烧电缆护套和绝缘材料释放的有毒气体会阻碍人员疏散和灭火活动。因此,本实验研究是为了调查韩国核电站使用的两种非1E级电缆的毒性。根据ISO 19702的标准规范对两种电缆进行了实验,测量了时间序列放热率、总放热率以及CO、CO2、HCl、HCN、HBr、HF、NOx、SO2等有毒气体的浓度。从实验结果可以看出,由于添加防火成分,放热率与排放气体中CO2的排放和少量卤化化合物的产生具有相似的特征。这些结果可作为评估电缆燃烧特性和人体毒性的基线数据。
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引用次数: 5
Combustion Instability Analysis of a Model Gas Turbine by Application of Dynamic Mode Decomposition 应用动态模态分解分析某型燃气轮机燃烧不稳定性
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2019-03-31 DOI: 10.15231/JKSC.2019.24.1.051
왕위엔강, J. Son, C. Sohn, Yoon Jisu, 배진현, Y. Yoon
Dynamic mode decomposition (DMD) technique is applied to analyze combustion instabilities in a model gas turbine combustor. The flame transfer function (FTF) obtained by the DMD method agrees with the experimental results qualitatively. However, FTF results show that the perturbation frequency with the largest gain is 100Hz, which contradicts the 1000Hz with the largest amplitude in the fast Fourier transform (FFT) results. In order to figure out this, gains and damping coefficients of all resonance frequencies are calculated by DMD technique. Results show the possibility that the model combustor has high-frequency instabilities as a results of coupling between flame and chamber responses. Another finding is that to obtain a pure FTF, the combustor must be removed to exclude coupling of chamber response with flame response.
采用动态模态分解(DMD)技术对模型燃气轮机燃烧室的燃烧不稳定性进行了分析。用DMD方法得到的火焰传递函数(FTF)与实验结果定性吻合。然而,FTF结果表明,增益最大的扰动频率为100Hz,这与快速傅里叶变换(FFT)结果中最大振幅为1000Hz的结果相矛盾。为此,利用DMD技术计算了各谐振频率的增益和阻尼系数。结果表明,由于火焰和燃烧室响应之间的耦合,模型燃烧室可能存在高频不稳定性。另一个发现是,为了获得纯粹的FTF,必须移除燃烧室以排除燃烧室响应与火焰响应的耦合。
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引用次数: 3
A 1-D Start-up Analysis for Liquid Rocket Engine Powerpacks 液体火箭发动机动力组的一维启动分析
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2019-03-31 DOI: 10.15231/JKSC.2019.24.1.039
Yu Seongha, Jo, Seonghwi, Kim, Hong-jip, 김성룡
A numerical study has been performed to investigate 1-D steady/unsteady start-up characteristics for liquid rocket engines using SINDA/FLUINT. First, in order to verify the analysis of cryogenic fluid, RL-10 engine having expander cycle is selected as a target of present study. Pressure drop in cooling channels was simulated through orifice devices. Satisfactory agreement has been obtained through the comparison of the numerical analysis and the experimental results. Based on these results, a start-up analysis of RD-8 having staged combustion cycle has been performed. As comparison of the numerical analysis and the experimental results, tendency of start-up characteristics had good agreements. This methodology of present study will be able to be used for the analysis of liquid rocket engines as a future work.
利用SINDA/FLUINT软件对液体火箭发动机的一维定/非定启动特性进行了数值研究。首先,为了验证低温流体的分析,选择具有膨胀循环的RL-10发动机作为本研究的目标。通过孔板装置模拟了冷却通道内的压降。通过数值分析与实验结果的比较,得到了满意的结果。在此基础上,对RD-8进行了分段燃烧循环的启动分析。数值分析结果与实验结果比较表明,启动特性的变化趋势符合较好。本研究的方法可作为今后液体火箭发动机分析的一项工作。
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引用次数: 1
A Hot Spot Based Shock to Detonation Transition Simulation using Multi-Scale Approach Part B - Hot Spot Based Multi-Scale Simulation - 基于热点的冲击-爆轰过渡多尺度模拟B部分——基于热点的多尺度模拟
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-12-31 DOI: 10.15231/jksc.2018.23.4.029
Yoocheon Kim, Jai-ick Yoh
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引用次数: 0
The Experimental Study about a Performance and Fine Particle Number Emissions with Several ETBE Contents and a Different Ignition Timing 几种ETBE含量和不同点火时间的性能和细颗粒数排放的实验研究
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-12-31 DOI: 10.15231/JKSC.2018.23.4.008
Ho-Young Song, Hongjip Kim
It has been known that oxygenates increase octane number of gasolines. There are MTBE and bio-ethanol known as typical oxygenates and a lot of increasing interests have been given to the researches on ETBE to alternate these oxygenates. In this study, the performance and emissions of fine particle number with changing ETBE contents and spark ignition timing in single cylinder engines have been studied. There were trends that oxygen contents and RON increased with increasing ETBE contents of gasolines. And the ignition delay became longer and the burning velocity was reduced with increasing oxygen contents. Net caloric value and RON of gasoline has affected BMEP and BSFC for various ignition timings. Knocking intensity sharply increased with advancing ignition timing, but the difference in the knocking intensity of high RON fuels was relatively low. And fine particle number emissions rapidly increased with advancing ignition timing.
众所周知,含氧化合物会增加汽油的辛烷值。MTBE和生物乙醇被称为典型的含氧化合物,人们对ETBE替代这些含氧化合物的研究越来越感兴趣。在本研究中,研究了单缸发动机细颗粒数随ETBE含量和火花点火正时变化的性能和排放。随着汽油中ETBE含量的增加,汽油中氧含量和RON有增加的趋势。随着氧含量的增加,点火延迟时间变长,燃烧速度降低。汽油的净热值和RON对不同点火时间的BMEP和BSFC有影响。爆震强度随点火时间的提前而急剧增加,但高RON燃料的爆震强度差异相对较小。随着点火时间的提前,细颗粒物排放量迅速增加。
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引用次数: 0
A Hot Spot Based Shock to Detonation Transition Simulation using Multi-Scale Approach Part A - Extraction of Chemical Kinetics of Energetic Material - 基于热点的多尺度冲击爆轰过渡模拟(A)——含能材料化学动力学的提取-
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-12-31 DOI: 10.15231/JKSC.2018.23.4.023
Yoocheon Kim, Jai-ick Yoh
Empirical and phenomenological hydrodynamic reactive flow models, such as Ignition and Growth and Johnson-Tang-Forest, have been effective in predicting shock initiation and detonation characteristics of various energetic substances. These models utilize the compression and pressure properties of the reacting mixture for quantifying their reaction rates. However, it has long been known that shock initiation of detonation is controlled by local reaction sites called ‘hot spots.’ In this study, a hot spot model based on the temperaturedependent Arrhenius reaction rate is developed. The complex reaction process of target explosive is addressed by conducting the Differential Scanning Calorimetry (DSC) while the rate of reaction is determined using the Friedman isoconversional method.
经验和现象学流体动力学反应流模型,如Ignition and Growth和Johnson-Tang-Forest,已经有效地预测了各种含能物质的激波起爆特性。这些模型利用反应混合物的压缩和压力特性来量化它们的反应速率。然而,人们早就知道,爆炸的冲击起爆是由称为“热点”的局部反应部位控制的。在这项研究中,建立了一个基于温度依赖的阿伦尼乌斯反应速率的热点模型。用差示扫描量热法(DSC)分析了目标炸药的复杂反应过程,用弗里德曼等转换法测定了反应速率。
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引用次数: 2
CFD Study on Combustion Chamber of Water-Tube Type Boiler with Dual Partial-Premixed Low NOx Burners 双部分预混低NOx燃烧器水管式锅炉燃烧室CFD研究
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-12-31 DOI: 10.15231/jksc.2018.23.4.039
Joon Ahn
A series of numerical simulations have been conducted for a combustion chamber of a water tube type boiler with dual partial-premixed burners. The burner was expected to give shorter flame to make the boiler be more compact. Two burners were predicted not to interact strongly so as to yield two semi-independent flames. 50% partial load operations were tried with 3 modes and the mode with lower burner was predicted to transfer heat to the combustion chamber most effectively.
对带有双部分预混燃烧器的水管式锅炉燃烧室进行了一系列数值模拟。期望燃烧器提供更短的火焰,使锅炉更紧凑。预计两个燃烧器不会强烈相互作用,从而产生两个半独立的火焰。试验了三种模式下的50%偏负荷运行,预测了低燃烧器模式能最有效地将热量传递到燃烧室。
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引用次数: 0
Combustion Instability Characteristics on Fuel Composition of a Partially-Premixed Flame 部分预混火焰燃料成分的燃烧不稳定特性
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-12-31 DOI: 10.15231/jksc.2018.23.4.015
W. Song, D. Cha, Byung Gu In
Combustion instability of synthetic gas in a partially-premixed combustor has been numerically investigated by varying H2 percentage of the fuel composition. During predictions with utilization of a lumped network code, the effects of different flame transfer function (FTF) models, which include the 2 order filter model and the state space model, and acoustic boundary conditions have also been investigated. The predicted results quite agree well with the corresponding experimental ones.
通过改变燃料成分中H2的百分比,对部分预混燃烧器中合成气的燃烧不稳定性进行了数值研究。在使用集总网络代码进行预测的过程中,还研究了不同火焰传递函数(FTF)模型的影响,包括二阶滤波器模型和状态空间模型,以及声学边界条件。预测结果与相应的实验结果吻合较好。
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引用次数: 3
A Study of a Premixed Methyl Decanoate/Air Flame under High Pressure 癸酸甲酯/空气预混高压火焰的研究
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-12-31 DOI: 10.15231/JKSC.2018.23.4.001
K. Lee
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引用次数: 1
A Study of the Effect of Diluted Hot Oxidant on MILD Combustion 稀释热氧化剂对轻度燃烧影响的研究
IF 0.4 Q4 ENGINEERING, MECHANICAL Pub Date : 2018-09-30 DOI: 10.15231/jksc.2018.23.3.043
C. Cha, H. Lee, S. Hwang
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引用次数: 0
期刊
Journal of the Korean Society of Combustion
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