球形压力容器中甲烷-氢气-空气爆炸过程数值模拟及实验研究

为研究受限空间内甲烷-氢气-空气混合气体爆炸特性参数分布规律,在20 L球形压力容器装置内开展甲烷-氢气-空气混合气体爆炸实验,探究掺氢比变化对当量比为1的甲烷-氢气-空气混合气体爆炸过程的影响;运用Fluent数值模拟软件,采用标准k-ε湍流模型,结合层流有限速率燃烧模型,探究混合气体爆炸过程中燃烧特性(爆炸温度、压力、密度等)与反应时间的变化规律。研究结果表明：爆炸过程中,添加一定氢气时爆炸压力峰值、爆炸压力上升速率峰值增大,而到达峰值时间缩短;反应初期,中心点火处密度下降,反应釜各处密度持续上升;距离点火点越远,密度变化越大,反应釜中压力分布基本相同。研究结果可为甲烷-氢气-空气混合燃料的安全使用提供相关参考。     

Flammability of kerosene in civil and military aviation

The investigation of the ignition conditions of kerosene vapors in the air contained in an aircraft fuel tank contributes to the definition of onboard safety requirements. Civil and military kerosene are characterized by specification. The specification of civil aviation kerosene is based upon usage requirements and property limits. while military kerosene is primarily controlled by specific chemical composition. Characterization of the flammability properties is a first step for the establishment of aircraft safety conditions. Flash point, vapor pressure, gas chromatography analysis, and flammability properties of the kerosene used by the French Military aviation (F-34 and F-35 kerosene) are compared with the flammability properties of civil kerosene. The empirical law established by the Federal Aviation Administration (FAA) in 1998, expressing the ignition energy in terms of fuel, temperature, flash point and altitude is modified and expressed in terms of fuel temperature, flash point and pressure.     

Analysis of the experimental results of the initiation of detonation in short tubes with kerosene–oxidizer mixtures

The paper describes the experimental investigation of detonation initiation in a mixture of kerosene–oxidant in a short test tube. Various mixtures of oxygen and nitrogen were used as an oxidant, from pure oxygen to the composition of air. The goal of the study was to determine the minimum diameter of the tube and the minimum level of energy needed for the direct initiation of detonation. As a result of the measurements the pressure courses were obtained for two kinds of cases: with and without (only shock waves) of fuel injection. The results of both kinds of measurements were compared, providing information about the initiation of detonation in a fuel–oxidizer mixture. Brief analyses of the results for different initiators and different oxidizers were performed and compared with the shock wave and Chapman–Jouget velocity.     

An experimental investigation of fluid flow and combustion characteristics of dual-fuel in a cylindrical combustion chamber

Combustion and fluid flow characteristics of coflowing LPG and kerosene have been investigated experimentally. A cylindrical water cooled combustion chamber was used to investigate the effect of changing the injection location and percentage of liquid fuel during gaseous fuel combustion. It was found that the injection of liquid fuel leads to an increase in the absolute value of maximum positive axial velocity and reduces the absolute value of the maximum negative axial velocity compared to the case of LPG alone. Also, a stable temperature distribution is noticed at axial distance of X/D approximately equal to 2.15 (where X is the axial distance measured from the inlet of diffuser, and D is chamber diameter). This is less than that of gaseous fuel combustion (approximately equal to 2.91). The change of injection location leads to a reduction in values of gas temperatures at X_inj/D=0.15 then it increased to reach maximum values at X_inj/D=0.35 which is approximately the same value for combustion of LPG fuel only. Any further increase in the injection location leads to a reduction in gas temperature, especially at the upstream sections of the combustion chamber. Also, it was found that values of temperature along the combustion chamber were decreased with increasing the percentage of the injected liquid fuel due to incomplete combustion of liquid fuel. Values of combustion chamber efficiency (η) for all percentage of liquid fuel at X_inj/D=0.35 are higher than those for combustion of LPG alone.     

Theoretical evaluation of lower explosion limit of hybrid mixtures

Lower explosion limits of hybrid fuel mixtures are usually determined through time consuming and expensive experiments. Although, mathematical expressions like Le-Chatelier's Law and Bartknecht curve have been used by many researchers to predict the LEL of hybrid mixtures, significant deviations remain unexplained. This research work, presents a more sophisticated and general approach for the determination of LEL of hybrid mixtures.Assuming that the combustion kinetics of pure species are independent and unchanged by the presence of other combustible species, complete conversion of the reactants and no heat losses, a simple mathematical model has been derived from the enthalpy balance of the whole system. For the experimental validation of the modelled values, modified version of 20L sphere has been employed, following the European standard (EN 14034-3: 2011) as experimental protocol. Hybrid mixtures of three dusts with two gases were selected for the scope of this publication. By analyzing the modelled as well as the experimental values, it can be concluded that the LEL values of the individual components in the hybrid mixture set the upper and lower limit for the LEL of the hybrid mixture provided the total amount of fuel in the system is considered as the concentration of the hybrid mixture. Moreover, the amount of dust or gas required to render the hybrid mixture flammable mainly depends on the energy contribution upon combustion of the individual species to raise the temperature of the whole system from ambient to the flame temperature.Le-Chatelier's Law and Bartknecht curve are empirical relations, which might hold true for a first-order approximation of LEL of hybrid mixtures, but do not represent the most conservative values of LEL reported in literature. This implies that there is a non-zero probability of occurrence of an explosible mixture in the non-explosible concentrations ranges defined by these relations. Considering these arguments, the authors suggest to employ the model presented in this paper – which presents reasonably conservative values of LEL of hybrid mixtures – for theoretical calculation of LEL of hybrid mixtures, when no precise experimental data is available.     

受限空间火灾轰燃过程的模拟实验研究

研制一种重现火灾轰燃的化学燃料和氧化剂的混合燃料，通过调整燃料的配方，可实现模拟控制火灾轰燃的温度和烟气产生量；实验研究了火灾轰燃过程烟气参数的变化规律，说明建筑火灾烟气运动的场-区-网模拟模型是合理的，分析了火灾过程中烟气的产生、运动、回流、下沉现象物理机制，指出在受限空间火灾救灾过程中应注意的问题。     

柴油汽车掺烧LPG降低黑烟排放技术

研究了柴油机掺烧液化石油气(LPG)以降低黑烟排放的技术方案，并开发出了一种以独特型板调节装置为特征的机械控制式柴油/LPG双燃料供给系统。发动机不改变原有结构加装该系统后即成为柴油/LPG双燃料发动机，可以同时燃烧柴油和LPG两种燃料，并且在整个工作范围内，随着工况变化能够按照预先优化设定的型板型线规律而自动调节柴油／LPG供给量比例，使烟度降低50％以上，同时满足经济性、动力性以及操作性能等要求，此外，也可以切换为单独燃烧柴油，而不改变发动机的原有性能。该系统结构简单、成本低廉，非常适合于改装城市在用公交车，降低其黑烟排放。     

Experimental investigation of spark ignition energy in kerosene,hexane, and hydrogen

Quantifying the risk of accidental ignition of flammable mixtures is extremely important in industry and aviation safety. The concept of a minimum ignition energy (MIE), obtained using a capacitive spark discharge ignition source, has traditionally formed the basis for determining the hazard posed by fuels. While extensive tabulations of historical MIE data exist, there has been little work done on ignition of realistic industrial and aviation fuels, such as gasoline or kerosene. In the current work, spark ignition tests are performed in a gaseous kerosene–air mixture with a liquid fuel temperature of 60 °C and a fixed spark gap of 3.3 mm. The required ignition energy was examined, and a range of spark energies over which there is a probability of ignition is identified and compared with previous test results in Jet A (aviation kerosene). The kerosene results are also compared with ignition test results obtained in previous work for traditional hydrogen-based surrogate mixtures used in safety testing as well as two hexane–air mixtures. Additionally, the statistical nature of spark ignition is discussed.     

楼梯井内烟囱效应对着火房间燃烧和溢出烟气的影响研究

实验研究了楼梯井内的烟囱效应对着火房间燃烧速率、补风速度、羽流温度等的影响.实验在一个模拟尺寸的十二层的楼梯井实验台内进行,实验时开启楼梯井顶层直通室外门.火灾时楼梯井内的烟囱效应加速了空气在楼梯井内的对流,使火源区从外界单侧卷吸空气,形成着火房间单侧强补风下的燃烧,燃烧速率比开放空间下的燃烧快,同时使得火焰向前室一侧倾斜,出现火焰"分岔"现象.与火源位于一层的工况相比,当火源位于六层,且首层门开启时,楼梯井内下部空气向上部烟气的掺混较大,着火房间门口进风速度减小,羽流的倾斜角度变小,温度较高,而当首层门关闭时,则减小了楼梯井下部空气与上部烟气的掺混,使得楼梯井内的上部烟气温度较高.     

Explosion behavior of hydrogen–methane/air mixtures

The effects of enriching natural gas with hydrogen on local flame extinction, combustion instabilities and power output have been widely studied for both stationary and mobile systems. On the contrary, the issues of explosion safety for hydrogen–methane mixtures are still under investigation.In this work, experimental tests were performed in a 5 L closed cylindrical vessel for explosions of hydrogen–methane mixtures in stoichiometric air. Different compositions of hydrogen–methane were tested (from pure methane to pure hydrogen) at varying initial pressures (1, 3 and 6 bar).Results have allowed the quantification of the combined effects of both mixture composition (i.e., hydrogen content in the fuel) and initial pressure on maximum pressure, maximum rate of pressure rise and burning velocity. The measured burning velocities were also correlated by means of a Le Chatelier’s Rule-like formula. Good predictions have been obtained (at any initial pressure), except for mixtures with hydrogen molar content in the fuel higher than 50%.     

CFD simulation of pressure piling

The explosion of flammable mixtures in interconnected compartments is commonly defined as “pressure piling”. Peak pressures much higher than the predictable thermodynamic values are likely to be generated in this geometry, yielding the phenomenon of major interest in industrial safety. In this paper, a CFD model was implemented, aiming at understanding the major factors affecting pressure piling in two cylindrical interconnected vessels, by varying the volume ratio between the two interconnected vessels and the ignition position. A combustion model was specifically developed to follow the flame propagation in any combustion regimes as a function of the local conditions: laminar, flamelet and distributed reaction zone.The model was validated by comparison with experimental results. The agreement between the experiments and the simulations has allowed the interpretation of the pressure piling phenomenon and the understanding of the mechanisms involved. More precisely, the results have showed that the pressure peak intensity is mainly affected by the coupling between the pre-compression of the mixture in the secondary vessel and the violence of explosion in the same vessel as related to the venting time, the latest quantified by the turbulent Bradley number, Br_t i.e. by the reaction time to the venting time ratio.     

油罐喷射火燃烧模拟

针对由一定压力的单相或两相介质泄漏或压力泄放系统排放引起的喷射火,利用gambit生成计算区域网格,得到相应的计算模型.再利用Fluent软件中的离散相模型计算气体流动,采用Realizable k-epsilon湍流模型和部分预混燃烧模型来预测燃料的燃烧,模拟了戊烷燃料燃烧和湍动多相流场,给出了燃烧速度矢量、温度和组...     

Experimental evaluation of the possibility of ignition and flame propagation in accumulated difluoromethane (R32) from a kerosene cigarette lighter

The possibility of ignition and flame propagation in accumulated difluoromethane (CH₂F₂, R32) was examined experimentally, simulating a situation in which a service operative uses a kerosene lighter for smoking. To simulate the situation where a kerosene cigarette lighter is used in accumulated R32, electrodes fixed in the windbreak of the lighter were remotely supplied with electricity to generate sparks of various durations but of similar energies to those of actual sparks generated by rubbing a flint to ignite the fuel in the lighter. We identified several cases of ignition and formation of an open flame in the windbreak of the lighter, and the flame propagated to the accumulated R32 when it was supplied with sufficient energy from the spark. Gas chromatographic analyses confirmed that the mixture in the windbreak of the kerosene lighter consisted mainly of vaporized fuel and air, with no R32. Therefore, even if the lighter is located in accumulated R32, an open flame can be generated in the windbreak of the kerosene cigarette lighter through ignition by the spark energy generated by friction between the flint and the flint wheel. Our results confirmed that there is a real possibility of ignition and flame propagation when a kerosene cigarette lighter is used in accumulated R32 under the leak rate conditions of the present experiment.     

Oxidation of kerosene components in a soil matrix by a dielectric barrier discharge reactor

This paper discusses some aspects of the kerosene components oxidation in a soil matrix by a dielectric barrier discharge reactor at atmospheric pressure. The total kerosene components abatement can reaches 90% for an energy density of 960 J g_soil^?1. The analyses of the discharge cell outlet gas reveals that CO_x and hydrocarbon compounds selectivity is close to 10%. A semi-quantitative approach by GC-FID shows that the carbon content in the oxidized compounds in soil is about 20% of the carbon content in the initial kerosene components. The polar species formed in soil are a mixture of aliphatic and aromatic molecules containing alcohol and carboxylic acid groups. The process of kerosene oxidation in soil matrix is more promoted than kerosene desorption followed by an oxidation in gas phase.     

低气压下火焰视频图像特征研究

为了进行非密封飞机机舱内视频火灾探测技术的研究,借助中国科学技术大学QR0-12步入式环境低气压试验舱开展低气压下(100kPa,90kPa,70kPa,50kPa和30kPa)火焰视频图像特征研究。在实验舱中用正庚烷作为可燃物进行点火实验,拍摄火焰视频,研究低气压环境下火焰的颜色、空间变化、运动、相对稳定性、边缘粗糙度、相邻帧火焰区域面积变化率、面积重叠率、相关性特征。实验结果表明,火焰的颜色、空间变化特征不会随气压变化而变化;而火焰动态特征等都会因气压的不同而发生变化。因此,火焰的颜色和空间变化特征在低气压环境中仍可用于火焰区域分割和识别,而其他动态特征会随着气压发生变化,不能用常压下的方法来训练分类模型,但仍可以用以区别火焰和静止的疑似区域。     

标准受限空间内细水雾熄灭煤油火的实验和数值模拟

在3.0m×3.0m×2.8m标准受限空间内,采用煤油模拟池火,火灾功率设定为195kW,进行了一系列细水雾灭火试验。对灭火时间做了详细记录,并实验研究了灭火时间的重现性及其相关因素。采用M-9000燃烧分析仪对细水雾施加前后火灾烟气(如氧气、二氧化碳、一氧化碳、一氧化氮、二氧化氮、二氧化硫)的浓度进行了在线测量。其结果表明:细水雾灭火系统熄灭煤油火的时间均在20s以内,灭火时间重现性保持在91.9%以内;施加细水雾后,氧气浓度降低,一氧化碳浓度升高,燃烧更加不完全。采用FDS模拟了细水雾熄灭煤油火,预测的温度场和灭火时间与实验结果吻合较好。     

Thermal radiation from vapour cloud explosions

The current study estimates the radiation flux emitted from hot extended gas clouds characteristic of vapour cloud explosions along with the corresponding level of irradiance posed on particles suspended in the unburnt part of the cloud ahead of an advancing flame front. The data presented permits an assessment of the plausibility of combustion initiation by such particles due to forward thermal radiation. The thermal radiation will depend on the emissivity of the burned volume, which relates to the concentration of gaseous and particulate combustion products. A sensitivity analysis has been carried out to account for variations in the equivalence ratio, mixture pressure and radiative heat losses. The spatial distribution of irradiance ahead of the flame front has been computed by introducing appropriate geometrical factors to explore the impact of cloud size. Using fuel rich ethylene-air mixtures it has been shown that high flame emissivities can be achieved at path lengths of order 1 m even in the presence of very low soot volume fractions. The emissivity of gas-soot mixtures will hence be mainly determined by the soot concentration and to a lesser extent by the mixture temperature. Our analysis suggests that the role of forward thermal radiation as a contributing factor to flame propagation in large scale vapour cloud explosions can not currently be ruled out.     

Numerical simulation of flame propagation and localized preflame autoignition in enclosures

A novel computational approach based on the coupled 3D Flame-Tracking–Particle (FTP) method is used for numerical simulation of confined explosions caused by preflame autoignition. The Flame-Tracking (FT) technique implies continuous tracing of the mean flame surface and application of the laminar/turbulent flame velocity concepts. The Particle method is based on the joint velocity–scalar probability density function approach for simulating reactive mixture autoignition in the preflame zone. The coupled algorithm is supplemented with the database of tabulated laminar flame velocities as well as with reaction rates of hydrocarbon fuel oxidation in wide ranges of initial temperature, pressure, and equivalence ratio. The main advantage of the FTP method is that it covers both possible modes of premixed combustion, namely, frontal and volumetric. As examples, combustion of premixed hydrogen–air, propane–air, and n-heptane–air mixtures in enclosures of different geometry is considered. At certain conditions, volumetric hot spots ahead of the propagating flame are identified. These hot spots transform to localized exothermic centers giving birth to spontaneous ignition waves traversing the preflame zone at very high apparent velocities, i.e., nearly homogeneous preflame explosion occurs. The abrupt pressure rise results in the formation of shock waves producing high overpressure peaks after reflections from enclosure walls.     

甲烷煤尘燃烧爆炸试验研究

为揭示甲烷煤尘空气混合物爆炸波的传播规律,采用试验分析的方法,建立甲烷煤尘空气混合物燃烧爆炸的3种试验方案,分析不同体积分数的甲烷和不同质量浓度的煤尘消耗不同体积空气时的爆压和爆速等参数的发展趋势,探究爆轰波传播的稳定性,阐明了甲烷煤尘燃烧爆炸的基本特征。试验结果表明,在最优配比条件下,与单一甲烷空气、煤尘空气混合物相比,甲烷煤尘空气混合物的爆压、爆速明显增加。甲烷煤尘空气混合物爆轰比单一的气相、固相混合物爆轰的爆炸压力、爆速明显增加、爆轰更稳定。     

Experimental study of the effect of nitrogen addition on gas explosion

Flame propagation and combustion characteristics of methane/air mixed gas in gas explosion were studied in a constant volume combustion bomb. Stretched flame propagation velocity, unstretched laminar flame propagation velocity, unstretched laminar combustion velocity and Markstein length were obtained at various ratios of nitrogen to gas mixture. Combustion stability at various ratios of nitrogen to gas mixture was analyzed by analyzing the pictures of flame propagation. Furthermore, the effect of initial pressure on the flame propagation and combustion characteristics of methane/air mixed gas in gas explosion was analyzed. The results show that the unstretched laminar flame propagation velocity, the unstretched laminar combustion velocity, Markstein length, flame stability, and the maximum combustion pressure decrease distinctly with the increase of nitrogen fraction in the gas mixture. At the same ratios of nitrogen to gas mixture, Markstein length, unstretched laminar flame propagation velocity and unstretched laminar combustion velocity decrease and the maximum combustion pressure increase with the increase of initial pressure of the gas mixture. When nitrogen fraction in the gas mixture is over 20%, the flame will be unstable and is easy to exterminate.