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1.
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.  相似文献   

2.
Deflagration phenomena in hydrogen–air mixtures initially filled in 1.4 m3 spherical latex balloons were measured using a high-speed digital video camera and pressure transducers. The image velocimetry using brightness subtraction was introduced to eliminate the background effects for obtaining accurate time evolution records of flame propagation velocity. The maximum flame propagation velocity of about 100 m/s was observed with maximum overpressure 15 kPa at 1 m from ignition point. According to the detailed flame propagation velocity records, there were long deceleration durations. The observed maximum overpressure was smaller than the overpressure estimated by the basis of the observed maximum flame propagation velocity and the pressure wave theories of spherical flames. A new blast curve plot of scaled overpressure vs. distance was tentatively proposed.  相似文献   

3.
The majority of experimental tests done on combustible dusts are performed in constant volume vessels that have limited or no optical access. Over the years, McGill University has been developing alternative experimental techniques based on direct observation of dust flames, yielding reliable fundamental parameters such as flame burning velocity, temperature and structure. The present work describes two new experimental set-ups allowing direct observation of isobaric and freely propagating dust flames at two sufficiently different scales to test the influence of scale on dust flame phenomena. In the laboratory-scale experiments, a few grams of aluminum powder are dispersed in transparent, 30 cm diameter latex balloons that allow for full visualization of the spherical flame propagation. In the field experiments, about 1 kg of aluminum powder is dispersed by a short pulse of air, forming a conical dust cloud with a total volume of about 5 m3. High-speed digital imaging is used to record the particle dispersal and flame propagation in both configurations. In the small-scale laboratory tests, the measured flame speed is found to be about 2.0 ± 0.2 m/s in fuel-rich aluminium clouds. The burning velocity, calculated by dividing the measured flame speed by the expansion factor deduced from thermodynamic equilibrium calculations, correlates well with the previously measured burning velocity of about 22–24 cm/s from Bunsen dust flames. Flame speeds observed in field experiments with large-scale clouds, however, are found to be much higher, in the range of 12 ± 2 m/s. Estimations are presented that show that the presumably greater role of radiative heat transfer in larger-scale aluminium flames is insufficient to explain the six-fold increase in flame speed. The role of residual large-eddy turbulence, as well as the frozen-turbulence effect leading to large-scale dust concentration fluctuations that cause flame folding, are discussed as two possible sources for the greater flame speed.  相似文献   

4.
为了研究油库常见的分支结构空间内发生油气爆炸时火焰和压力的传播特性,建立了基于WALE湍流模型及Zimont预混火焰模型的油气爆炸模型;模拟了6种不同分支管道结构空间内汽油/空气混合物爆炸发生发展过程;研究了分支管道数量及相对设置位置对爆炸超压的影响规律,以及分支管道对火焰传播形态和速度的影响规律;模拟结果与前人相关实验规律进行对比。研究结果表明:分支管道对汽油/空气混合气预混爆炸具有明显的强化激励作用;火焰锋面传播经过分支管道时,经历规则—褶皱—规则的变化过程;主管道内火焰传播速度,在分支管道对流场的突扩作用和湍流作用的共同影响下呈震荡变化的规律。  相似文献   

5.
为了揭示空气中丙烷火焰传播特性,利用纹影系统记录了预混气体小能量点火条件下火焰形成与传播过程,得到了火焰表面的微观结构特征,分析了混合气体火焰的稳定性及其影响因素。结果表明:丙烷/空气混合物火焰发展过程及其表面微观特征与浓度直接相关;当混合物浓度接近爆炸上下限时,火焰扩展速率整体不大于0.5 m/s,燃烧区域向上漂浮,浮力成为影响火焰失稳的主导因素;当混合物浓度靠理论配比时,火焰呈规则球形扩展,火焰稳定性按照先减弱后增强的趋势发展,火焰表面褶皱的形成及演化规律是热扩散不稳定性和流体力学不稳定性共存与竞争的作用结果。  相似文献   

6.
为了研究分岔管道不同封闭状态下瓦斯爆燃火焰阵面传播规律,在自制的T型透明分岔管道内,设置支管端口完全封闭、直管左端口弱封闭,采用光电传感器和压力传感器测试了直管右端弱封闭、完全封闭2种情况下,预混甲烷-空气可燃气体爆燃火焰传播过程中速度、超压参数的变化情况。结果表明:由于分岔的存在,2种封闭状态在支管端点火后瓦斯爆燃火焰阵面在支管中的传播速度均先增大后减小;直管右端弱封闭时,经过分岔后火焰加速向直管两端传播速度基本一致,分别达到86.29 m/s和88.07 m/s;直管右端完全封闭时,火焰向弱封闭端传播速度增大至166.67 m/s,火焰向完全封闭端传播时并不断压缩未燃气体产生高压振荡反馈导致火焰振荡传播现象,火焰速度不断减小至4.84 m/s;管道内瓦斯爆燃超压均迅速上升到达峰值,之后受压缩气体的膨胀和冲击后爆燃产物的振荡作用迅速下降。  相似文献   

7.
为研究多孔材料对封闭管道内甲烷-空气预混气体火焰传播的影响,设计加工了横截面积为80 mm×80 mm的方形试验管道,运用自发光拍摄技术和动态压力传感器对甲烷-空气预混火焰在该管道内传播过程中形状变化和压力特性进行了实验研究。结果表明,在管道尾部放置3种不同材质的多孔材料时,其对爆炸压力均有一定的抑制作用,聚氨酯泡沫对管道内压力的衰减效果优于聚苯乙烯泡沫和自制泡沫材料。对压力曲线进行一次求导,得出了压力变化速率,结果与空管道实验相比,在放置多孔材料的管道内压力降低的速率更快,时间更短。  相似文献   

8.
An experimental study has been conducted to investigate the effects of hydrogen addition on the fundamental propagation characteristics of methane/air premixed flames at different equivalence ratios in a venting duct. The hydrogen fraction in the methane–hydrogen mixture was varied from 0 to 1 at equivalence ratios of 0.8, 1.0 and 1.2. The results indicate that the tendency towards flame instability increased with the fraction of hydrogen, and the premixed hydrogen/methane flame underwent a complex shape change with the increasing hydrogen fraction. The tulip flame only formed when the fraction of hydrogen ranged from 0 to 50% at an equivalence ratio of 0.8. It was also found that the flame front speed and the overpressure increased significantly with the hydrogen fraction. For all equivalence ratios, the stoichiometric flame (Φ = 1.0) has the shortest time of flame propagation and the maximum overpressure.  相似文献   

9.
The structure of flame propagating through lycopodium dust clouds has been investigated experimentally. Upward propagating laminar flames in a vertical duct of 1800 mm height and 150×150 mm square cross-section are observed, and the leading flame front is also visualized using by a high-speed video camera. Although the dust concentration decreases slightly along the height of duct, the leading flame edge propagates upwards at a constant velocity. The maximum upward propagating velocity is 0.50 m/s at a dust concentration of 170 g/m3. Behind the upward propagating flame, some downward propagating flames are also observed. Despite the employment of nearly equal sized particles and its good dispersability and flowability, the reaction zone in lycopodium particles cloud shows the double flame structure in which isolated individual burning particles (0.5–1.0 mm in diameter) and the ball-shaped flames (2–4 mm in diameter; the combustion time of 4–6 ms) surrounding several particles are included. The ball-shaped flame appears as a faint flame in which several luminous spots are distributed, and then it turns into a luminous flame before disappearance. In order to distinguish these ball-shaped flames from others with some exceptions for merged flames, they are defined as independent flames in this study. The flame thickness in a lycopodium dust flame is observed to be 20 mm, about several orders of magnitude higher than that of a premixed gaseous flame. From the microscopic visualization, it was found that the flame front propagating through lycopodium particles is discontinuous and not smooth.  相似文献   

10.
为研究调节风窗的面积、位置对瓦斯爆炸传播特性的影响,通过FLACS软件构建不同面积和不同位置调节风窗的风门-巷道模型,对瓦斯在该模型中的爆炸及其传播进行数值模拟,并分析瓦斯爆炸压力、火焰传播速度。研究结果表明:风门前最大瓦斯爆炸压力值与调节风窗边长呈现指数减小关系,而风门后最大瓦斯爆炸压力值与调节风窗边长呈现指数增加关系;火焰传播速度与调节风窗边长呈现指数增加关系;相同面积情况下,调节风窗中心位置对瓦斯爆炸影响较小。  相似文献   

11.
Experimental studies were done with a small pipe with a diameter of 0.043 m and a large pipe with a diameter of 0.49 m to demonstrate the flame propagation suppression with inertia isolation in a long duct. Tests were carried in an ignition section containing propylene/air mixture near stoichiometric concentration and generating a peak flame propagation speed of approximately 100 m/s. The ignition section is connected to a section filled with an inert gas, another section with flammable mixtures, and finally a sufficiently long, ambient section to accommodate flame propagation. The critical length of the inert gas section required for successful suppression of flame from the igniting the flammable section is found to be 0.6 m for CO2 and 0.9 m for N2 in the large pipe and 0.2 m for CO2 and 0.3 m for N2 in the small pipe. Additional tests with a 3 m of ignition section and peak flame propagation speed of 225 m/s showed that the critical length for successful suppression by CO2 is only increased slightly to 0.9 m, confirming that the suppression is a result of inertia isolation rather than inert gas dilution. Finally, application of the results in responding to large-scale leak into a long, underground duct is discussed.  相似文献   

12.
This paper presents a new model of explosion propagation in a closed vessel. The foundation of the formulation is a sub-model of turbulent burning velocity based on the assumption that the burning velocity of a turbulent wrinkled flame can be determined from the flame surface. In addition, model development includes simple sub-models of heat transfer and free convection. In order to verify the physics, the model was utilized to simulate the explosion of a methane–air mixture in two different test vessels. The results obtained by use of this new model were compared with results obtained by use of the classical model. While the simulations showed that both are accurate, the new model presented in this paper (called “flame surface model” for simplicity) is more flexible and can easily accommodate sub-models of different phenomena that can play an important role in fuel–air explosions.  相似文献   

13.
路长  李毅  潘荣锟 《火灾科学》2015,24(2):68-74
为研究管道截面对氢气/空气预混火焰形状与传播速度的影响,选用三个长度都为1m而截面尺寸不同的方形管道进行实验。实验结果表明,在截面为80mm×80mm的管道中,四种氢气浓度下预混火焰都发展形成了郁金香火焰。火焰传播速度呈现上升,下降,再上升的波动。在截面为100mm×100mm和150mm×150mm的管道中,只有在氢气浓度20%下形成郁金香火焰,并且传播速度也出现上述的波动。而在氢气浓度25%,30%,40%下,预混火焰都呈指尖形传至管口,未出现郁金香火焰,传播速度都是不断上升。三个管道对比中,截面为100mm×100mm的管道内火焰平均传播速度最快,且压力波第一峰值最大。  相似文献   

14.
Correlating turbulent burning velocity to turbulence intensity and basic flame parameters-like laminar burning velocity for dust air mixtures is not only a scientific challenge but also of practical importance for the modelling of dust flame propagation in industrial facilities and choice of adequate safety strategy. The open tube method has been implemented to measure laminar and turbulent burning velocities at laboratory scale for turbulence intensities in the range of a few m/s. Special care has been given to the experimental technique so that a direct access to the desired parameters was possible minimising interpretation difficulties. In particular, the flame is propagating freely, the flame velocity is directly accessible by visualisation and the turbulence intensity is measured at the flame front during flame propagation with special aerodynamic probes. In the present paper, those achievements are briefly recalled. In addition, a complete set of experiments for diametrically opposed dusts, starch and aluminium, has been performed and is presented hereafter. The experimental data, measured for potato dust air mixtures seem to be in accordance with the Bray Gülder model in the range of 1.5 m/s<u′<3.5 m/s. For a further confirmation, the measurement range has been extended to lower levels of turbulence of u′<1.5 m/s. This could be achieved by changing the mode of preparation of the dust air mixture. In former tests, the particles have been injected into the tube from a pressurised dust reservoir; for the lower turbulence range, the particles have been inserted into the tube from above by means of a sieve–riddler system, and the turbulence generated from the pressurised gas reservoir as before. For higher levels of turbulence, aluminium air mixtures have been investigated using the particle injection mode with pressurised dust reservoir. Due to high burning rates much higher flame speeds than for potato dusts of up to 23 m/s have been obtained.  相似文献   

15.
市政排污空间作为城市公共基础设施的重要组成部分,易积聚可燃气体形成爆炸性环境。结合排污空间的特殊环境条件,采用Fluidyn-MP多物理场数值模拟软件,建立了20 L球形爆炸罐分析模型,通过改变初始温度和初始压力,对排污空间甲烷-空气混合物爆燃特性及其变化规律进行模拟研究。结果表明:初始温度升高导致甲烷-空气混合物最大爆炸压力降低,缩短了到达最大爆炸压力的时间;初始压力增加导致最大爆炸压力急剧升高,并延长了到达最大爆炸压力的时间;最大爆炸压力对初始压力的敏感程度远大于初始温度的影响。此外,随着初始温度和初始压力的升高,爆炸火焰平均传播速度增加,而火焰传播速度对初始温度较敏感。  相似文献   

16.
为研究惰性气体抑制瓦斯爆燃火焰传播特性,在自行搭建的中尺度爆炸激波管道上,采用数据采集系统、压电式传感器、火焰传感器、同步控制系统和激光纹影测试系统,通过对比4种不同喷射压力(0.5,1.5,2.5,3.5 MPa)的实验工况,选用N2做为惰性介质时抑制火焰的传播特性与喷射压力密切相关,火焰传播速度随着喷射压力增加呈现先增加后减弱的趋势。研究结果表明:少量N2在管道中扩散,加剧了未反应预混气体的扰动状态,造成火焰阵面褶皱的卷吸能力增强,进而加速化学反应进程,促进预混气体燃烧;喷射压力为1.5 MPa时,火焰阵面拉升、变形最强,火焰传播速度提高,最高可达到250 m/s;喷射压力为3.5 MPa时,火焰阵面出现明显三维凹陷结构,运动发生明显滞后现象,火焰传播速度大幅度降低至5.4 m/s,惰性气体抑制火焰传播效果明显。  相似文献   

17.
Flame behavior and blast waves generated during unconfined hydrogen deflagrations were experimentally studied using infrared photography. Infrared photography enables expanding spherical flame behaviors to be measured and flame acceleration exponents to be evaluated. In the present experiments, hydrogen/air mixtures of various concentrations were filled in a plastic tent of thin vinyl sheet of 1 m3 and ignited by an electric spark. The onset of accelerative dynamics on the flame propagation was analyzed by the time histories of the flame radius and the stretched flame speed. The results demonstrated that the self-acceleration of the flame, which was caused by diffusional-thermal and hydrodynamic instabilities of the blast wave, was influenced by hydrogen deflagrations in unconfined areas. In particular, it was demonstrated that the overpressure rapidly increased with time. The burning velocity acceleration was greatly enhanced with spontaneous-turbulization.  相似文献   

18.
为研究管道内金属丝网对甲烷/空气预混火焰传播的影响,通过实验和三维数值模拟研究安装金属丝网的管道内火焰传播特性以及流场、温度场的变化。结果表明:40目4层的金属丝网可以使火焰淬熄,30目4层的金属丝网无法淬熄,但可以使火焰停滞3 ms;大涡模型可以很好地对管道内火焰淬熄现象进行模拟;当火焰穿过30目4层金属丝网时,速度增大,在Kelvin Helmholtz不稳定和Rayleigh Taylor不稳定的耦合作用下形成湍流;金属丝网的目数会影响热量在丝网层中的扩散,当金属丝网为30目4层时,火焰热量扩散快,而当金属丝网为40目4层时,火焰热量扩散慢且温度大幅度衰减,衰减率达到83%。  相似文献   

19.
Experiments about the influence of ultrafine water mist on the methane/air explosion were carried out in a fully sealed visual vessel with methane concentrations of 8%, 9.5%, 11% and 12.5%. Water mists were generated by two nozzles and the droplets' Sauter Mean Diameters (SMD) were 28.2 μm and 43.3 μm respectively which were measured by Phase Doppler Particle Anemometer (PDPA). A high speed camera was used to record the flame propagation processes. The results show that the maximum explosion overpressure, pressure rising rate and flame propagation velocity of methane explosions in various concentrations increased significantly after spraying. Furthermore, the brightness of explosion flame got much higher after spraying. Besides, the mist with a larger diameter had a stronger turbulent effect and could lead to a more violent explosion reaction.  相似文献   

20.
为研究不同封闭情况下T型管道中瓦斯爆炸的传播规律,在90°分岔管道中进行瓦斯爆炸实验,管道封闭情况为弱封闭(双PVC薄膜弱封闭)和强封闭(直管封闭或支管封闭)。实验结果表明:在瓦斯浓度为9.5%时,管道中各点处的瓦斯爆炸压力、火焰传播速度和火焰锋面振荡幅度最大,11%次之,8%最小。T型管道中,弱封闭端瓦斯爆炸压力不断减小;火焰传播速度先缓慢增大后减小,随后又快速增大。强封闭端,瓦斯爆炸压力增大;火焰传播速度先缓慢增大后略微下降,随后快速增大后又大幅度下降,甚至出现火焰锋面振荡现象。不同封闭管道中各测点的瓦斯最大爆炸压力和火焰传播速度大小比较可知,直管封闭管道>双PVC薄膜弱封闭管道>支管封闭管道。  相似文献   

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