Z型管道中气体火焰传播规律的实验研究

本文实验研究了丙烷／氧气／空气的当量比气体燃烧火焰通过两个90°弯管形成的“z”型管道的传播规律,通过改变第一个弯管前加速段的长度和改变气体浓度,实验研究了稳定爆轰波,非稳定爆轰波以及爆燃火焰通过“z”型管道的传播规律。利用光电传感器记录弯管前后的火焰传播速度,运用燃烧理论和爆轰波的理论对实验结果做了分析。结果表明:稳定爆轰波通过“z”型管道时传播速度有明显的下降;但“z”型管道对非稳定爆轰波的传播作用受到非稳定爆轰波自身速度的影响;爆燃火焰通过“z”型管道时火焰传播速度的变化呈现不确定性。     

爆炸性气体在连续拐弯管道中传播特性的实验研究

针对复杂燃气管网燃气爆炸致灾严重,传播规律复杂的问题,利用实验室加工成的连续拐弯管道,模拟研究了复杂燃气管网爆炸性气体通过连续拐弯管道时的火焰传播速度、爆炸波超压变化情况。研究结果表明,当整个管道内充满瓦斯气体时,通过连续拐弯后,火焰传播速度和爆炸波超压值产生显著变化,在连续拐弯管道拐弯处为一扰动源,诱导附加湍流,气流湍流度增大,管道拐弯增加了燃烧区的湍流度,火焰燃烧产生加速度,加速燃烧产生更大能量以推动加速传播。研究结果对指导现场如何防治复杂燃气管网气体爆炸,减轻爆炸的威力具有重要作用。     

大长径比管道汽油-空气混合气爆炸与抑制实验研究*

为探究狭长受限空间中油气爆炸失控时的发展状态,探索高效环保的油气爆炸抑制方法,利用长径比155的管道开展92号汽油-空气混合气爆炸发展规律和七氟丙烷主动抑爆技术研究。通过测量不同端部开口条件下油气爆炸超压、火焰传播速度、火焰强度等参数,对比研究空爆和抑爆工况下的油气爆炸变化规律,探讨长直管道中的油气爆炸特性,分析七氟丙烷抑爆效果。结果表明:大长径比管道中,端部开口泄爆对降低油气爆炸破坏能力的作用较小,开口与否对最大超压峰值的出现位置有影响;长直管道空爆时,油气爆炸由爆燃发展成爆轰,管道尾部的爆轰波速可达近2 000 m/s;密闭管道中,爆轰发生前火焰传播呈“已燃区-火焰锋面-待燃区-前驱激波-未燃区”的2波3区结构;主动抑爆方式下七氟丙烷抑爆效果良好,最大超压峰值降低幅度可达90%,火焰传播被及时阻断。     

爆炸形成过程中火焰加速的试验研究

为预防和控制工业爆炸事故,并为脉冲爆轰发动机的研究提供理论指导,分析火焰加速导致的燃烧转爆轰过程的影响因素。采用爆轰管探讨障碍物的阻塞比、混合物的组成、初始压力和点火能等4个因素对爆炸性气体火焰速度和爆轰压力的影响规律。试验结果表明:障碍物的存在能大大提高火焰速度和爆轰压力;爆轰压力随管内障碍物阻塞比的增大先变大后减小,并在阻塞比为0.498,燃料种类为天然气,化学当量比为1时达到最大;爆轰压力还随混合气体初始压力的增大和点火能的提高而增大。选择适宜的条件可大大提高火焰加速速率,促进燃烧向爆轰过程转变。     

气相爆轰实验系统设计

设计了一套内径139 mm、总长10 m的气体、粉尘爆轰管道式反应装置,装置由试验管道系统、测试系统、辅助实验系统和控制系统4部分构成。测试系统包括高频响动态压力传感器、火焰传感器、超动态应变仪、数据采集卡、高速摄像系统等设备,以便测试可燃气体、粉尘的爆轰参数和管道的动力学响应特征参数。实验装置可用于可燃气云和粉尘的燃烧、爆炸特性以及爆轰波对结构加载作用的研究,研究成果可用于燃气输送管道的设计、校核,为安全生产保驾护航。     

瓦斯爆炸过程中火焰瞬时传播规律研究

在改善后的瓦斯爆炸试验条件下,为了得到任意位置的火焰传播速度,对火焰通过各传感器所处的位置与其对应时间进行统计分析,发现可以用二次抛物线方程来表达火焰传播距离与其对应时间之间的关系,由此推导火焰瞬时传播速度随管道位置变化的关系式,得到管道任意位置及任意时刻的火焰速度计算公式。研究发现:瓦斯爆炸火焰传播运动过程近似于匀加速直线运动过程;当加螺旋环时火焰传播过程接近于匀速直线运动。随着管道长度的不断增大,火焰瞬时速度不断增加,但增加的幅度越来越小,当管道长度达到某值后,火焰速度将趋于某一定值。煤矿井下可根据各点计算得出的火焰速度大小,采用相应的预防措施,减少瓦斯爆炸造成的损失。     

球形障碍物对瓦斯爆燃火焰影响试验研究

为进一步开发煤矿井下瓦斯爆炸事故的隔抑爆技术装备,利用截面为0.2 m×0.2 m的方形管道、纹影仪和高速摄像机,开展无障碍物时和球形障碍物存在情况下的瓦斯爆燃传播试验。研究发现,无障碍物时,密闭管道内爆燃火焰的结构和传播速度受反射压力波的影响很大,湍流火焰、化学反应作用能力与反射压力波的相互作用是造成火焰传播速度变化的主要原因;球形障碍物存在时,火焰受扰动后被拉伸为前锋、中锋和尾锋,前锋速度最快,尾锋最慢;火焰前锋从经过障碍物开始整体呈加速趋势,与无障碍物相比,通过观察段的时间明显缩短。     

氢气爆燃转爆轰特性试验研究

为揭示爆燃转爆轰(DDT)过程的主要物理机理,用带有Shchelkin螺纹管的方形激波管,对氢气和空气混合气进行爆轰试验。首先采用压力传感器记录压力波在管内的发展过程,探讨压力波速度的变化规律;然后借助高速照相机获得DDT转捩过程的纹影图像,分析主导激波传播速度的变化规律。结果表明,火焰传播经历缓燃、爆燃、爆燃转强爆轰、强爆轰衰减以及稳定爆轰等阶段;火焰、主导激波和反射激波间的相互作用是影响DDT转捩过程的主要因素。采用压力-时间记录法和纹影法分别得到DDT距离,但用后者所得的转捩距离更为准确。     

网状金属材料对火焰波阻隔作用的实验研究

为了研究网状金属材料对火焰波的阻隔作用,设计了可架设阻隔材料的气体爆炸箱,借助高速摄像机及ProAnalyst软件,测定了不同点火位置、不同网状金属材料条件下的气体爆炸后火焰波运动状态,进而分析了网状金属材料在该条件下对火焰波的阻隔作用。实验表明:在无阻隔物时,气体爆炸后的火焰波以球形向四周传播,其速度趋势呈抛物线形变化,存在一个速度的峰值;设置阻隔物后,火焰波遇阻隔物发生形变,垂直于阻隔物方向速度峰值降低,但同时水平方向传播速度加快,阻隔物距离点火源越近,这些现象越明显;在相同点火距离下,对于不同金属的阻隔物,火焰波垂直方向传播速度及其峰值以及到达峰值的时间与材料的导热系数具有负相关性。可见,从位置上看,阻隔物靠近点火源,可以有效阻隔垂直火焰波;从材料上看,选择导热系数大的金属阻隔材料,不但可以有效阻隔垂直火焰波,还可以使阻隔作用提前,起到双重的阻隔效果。     

连通器内预混气体泄爆过程的数值模拟

连通器内预混爆炸性混合气体被点燃后,随着气体燃烧火焰的传播,而发展成爆轰,压力急剧上升,故研究连通器安装爆破片后,泄爆过程的数值模拟有其重要价值.采用有限元的方法,对连通器内预混气体的火焰传播和泄爆过程进行数值模拟.通过模拟获得了不同时刻燃爆的速度场、密度场、浓度场、温度场,为工程上防爆、抑爆、泄爆提供了理论基础和数据.     

Flame acceleration in pipes containing bends of different angles

Bend structures are common in process industries. These bends containing three typical angles (90°, obtuse angle and acute angle) are often incorporated into pipes or ducts at different positions. In our experiments, the effect of both the bend angle and bend position on flame acceleration was studied. Flame acceleration in a pipe bend can be divided into three stages. The flame speeds increased before the bend and increased again after decreasing for a short distance in the bend. Flame reversing decreased the flame speeds in the bend and led to additional turbulence, which enhanced flame acceleration after the bend. The flame acceleration in three different pipe bend angles had similar trends. The decreasing amplitude of the flame speed in the bend increased with a decrease in the bend angles. The flame speeds in the bend were ordered such that 52° <90° <145°. However, the maximum flame speeds in the pipe were in the opposite order. Additionally, both the flame speeds in the bends and the maximum flame speeds in the whole pipes increased as the bend’s position away from ignition point increased.     

An experimental study of flame acceleration and deflagration to detonation transition in representative process piping

The paper summarizes the results of experimental tests and accompanying analyses to investigate the factors that govern flame acceleration and potential transition to detonation in a relatively long unobstructed piping system. The overall aim of the work was to obtain sufficient experimental data so as to be able to develop and evaluate methodologies for classifying and predicting potential detonation flame acceleration and deflagration to detonation transition (DDT) hazard in industrial process pipes and mixtures. The present results show that the flame acceleration process in an unobstructed pipe exhibit three distinct phases: an initial establishment phase; a second rapid acceleration phase and a final transition to detonation phase. Test results with ethylene indicate that the acceleration process is not sensitive to initial pressure (all other parameters remaining constant) but can be sensitivity to initial pipe wall temperature or possibly mixture humidity. The presence of bends increases the local rate of turbulent combustion, an effect attributed to the additional turbulence generated downstream of the bend. For straight pipes, detonation was only observed to develop for hydrogen–air and ethylene–air mixtures. Detonation was not observed with methane, propane or acetone as fuel in the present piping apparatus.     

Efficient simulation of flame acceleration and deflagration-to-detonation transition in smooth pipes

Evaluation of accident scenarios including flame acceleration and deflagration-to-detonation transition (DDT) in chemical plant piping systems increases the need for an efficient numerical simulation tool capable of dealing with this phenomenon. In this work, a hybrid pressure-density-based solver including deflagrative flame propagation as well as detonation propagation is presented. The initial incompressible acceleration stage is covered by the pressure-based solver until the flame velocity reaches the fast flame regime and transition to the density-based solver is done. The deflagration source term is formulated in terms of a turbulent flame speed closure model incorporating various physical effects crucial for flame acceleration at low turbulence conditions (Katzy and Sattelmayer, 2018). Modelling of the detonation source term is based on a quadratic heat release function (Hasslberger, 2017). The presented numerical approach is validated in terms of DDT locations and pressure data from Schildberg (2015) as well as recently completed flame tip position measurements. For this purpose, H₂/O₂/N₂ mixtures ranging from 25.6 vol-% H₂ to 29.56 vol-% H₂ in two different pipe geometries are considered. The focus of the current work is on predicting the DDT location correctly and good agreement is observed for the investigated cases.     

管道内瓦斯爆炸传播的试验研究

运用大型试验管道对瓦斯爆炸传播规律进行试验研究,并对瓦斯爆炸压力峰值、火焰速度和呈现时间进行分析,得出:在不出现爆轰的前提下,爆源点附近的压力峰值是全管道的最大值;爆炸压力峰值在沿管道的传播过程中从爆源点附近是先增大后减小,然后再逐渐增大且压力峰值最早呈现在出口附近;火焰传播速度随着传播距离的增大而逐渐增大且在爆炸初期增大速率更快;瓦斯浓度对爆炸压力峰值、火焰传播速度和呈现时间等都有重要影响。     

Numerical simulation of flame acceleration and deflagration-to-detonation transition of ethylene in channels

Ethylene (C₂H₄) is a hydrocarbon fuel and widely used in chemical industry, however, ethylene is highly flammable and therefore presents a serious fire and explosion hazard. This work is initiated by addressing the hazard assessment of ethylene mixtures in different scale channels (d = 5 mm, 10 mm and 20 mm) from the aspect of flame acceleration (FA) and deflagration-to-detonation transition (DDT) by using large eddy simulation (LES) method coupled with the artificially thickened flame (ATF) approach. The fifth order local characteristics based weighted essentially non-oscillatory (WENO) conservative finite difference scheme is employed to solve the governing equations. The numerical results confirm that flame velocity increase rapidly at the beginning stage in three channels, and the flame acceleration rate is slower in the subsequent stage, afterwards, the flame velocity has an abrupt increase, and the onset of detonation occurs. Due to the fact that wall effect is significant in the narrow channel (e.g.,5 mm), especially in the ignition stage of the flame, flames have different shapes in wider channels (10 mm and 20 mm) and narrow channel (5 mm). Both the pressure and temperature profiles confirm DDT run-up distances are 0.251 m, 0.203 m and 0.161 m in 20 mm, 10 mm and 5 mm channels, respectively, which indicates that a shorter run-up distance is required in narrower channel. The cellular detonation structures for the ethylene-air mixture in different channels indicate that multi-headed detonation structures can be found in 20 mm channel, as the channel width decreases to 10 mm, detonation has a single-headed spinning structure, as the width is further reduced to 5 mm, only large longitudinal oscillation of the pressure can be observed.     

High resolution numerical simulation of methane explosion in bend ducts

In this paper we developed a parallel code, adopting a fifth-order weighted essentially non-oscillatory (WENO) scheme with a third-order TVD Runge-Kutta time stepping method for the two-dimensional reactive Euler equations, to investigate the propagation process of methane explosion in bend ducts. In the simulations, an inverse Lax-Wendroff procedure is adopted to construct a high order boundary in order to treat the complex boundaries. The numerical results show that when the bend angle is 30° and 45°, it cannot inhibit the propagation of the detonation wave; while when the angle reaches 60° and 75°, the detonation wave finally attenuates to the shock wave. It indicates that the propagation of the detonation wave can be inhibited. Furthermore, the temperature and the pressure at the entrance of the bend are low. When the angle arrives at 90°, the detonation wave evolves into cellular detonation when it passes through the bend. When the angle is larger than 90°, the detonation wave dramatically attenuates at the diffracting point, and later some hot spots can be formed, which can ignite the combustible gas nearby. Thus the second explosion occurs and finally the detonation is formed. When the angle is larger than or equal to 90°, the temperature and the pressure at the entrance of the bend is too high that the rescue efforts in the methane explosion accidents will encounter great difficulties. Hence, the laneway with 60° and 75° bend can inhibit the propagation of the detonation wave, and the temperature and the pressure at the entrance of the bend is not too high as well. All the results above can provide an important basis for the design and optimization of the mine laneway.     

Explosions in closed pipes containing baffles and 90 degree bends

There is a general lack of information on the effects of full-bore obstacles on combustion in the literature, these obstacles are prevalent in many applications and knowledge of their effects on phenomena including burning rate, flame acceleration and DDT is important for the correct placing of explosion safety devices such as flame arresters and venting devices. In this work methane, propane, ethylene and hydrogen–air explosions were investigated in an 18 m long DN150 closed pipe with a 90 degree bend and various baffle obstacles placed at a short distance from the ignition source. After carrying out multiple experiments with the same configuration it was found that a relatively large variance existed in the measured flame speeds and overpressures, this was attributed to a stochastic element in how flames evolved and also how they caused and interacted with turbulence to produce flame acceleration. This led to several experiments being carried out for one configuration in order to obtain a meaningful average. It was shown that a 90 degree bend in a long tube had the ability to enhance flame speeds and overpressures, and shorten the run-up distance to DDT to a varying degree for a number of gases. In terms of the qualitative effects on these parameters they were comparable to baffle type obstacles with a blockage ratios of between 10 and 20%.     

Decomposing detonation and deflagration properties of ozone/oxygen mixtures

In this study, the decomposing detonation and deflagration properties of ozone/oxygen mixtures of up to 20 vol.% of ozone in oxygen under high pressure of up to 1.0 MPa in a tube were experimentally investigated. The mixtures were ignited by an electric spark at the end of the tube. Flame propagation properties such as flame velocity and pressure were measured with thermocouples and piezo electric transducers mounted along the tube. Slow and constant flame propagation profiles were obtained. We also investigated the quenching ability of a wire gauze as well as the concentration limit for flame propagation. However, in spite of slow flame propagation velocity and easy flame quenching properties under these experimental conditions, direct initiation of detonation by the driver detonation of the stoichiometric oxy-hydrogen mixture was easily achieved at much lower concentrations than the limit of deflagration. The observed detonation properties, such as wave velocity and pressure, agreed fairly well with C–J calculated values. The detonation velocity (900–1200 m/s) and the pressure ratio to initial pressures (5–9.5) were not affected by the initial pressure of the mixtures. Near the detonation limit, typical spinning detonations with oscillatory pressure waves were observed.