气体爆轰波在弯曲管道中传播特性的实验研究

对丙烷 -空气爆轰波通过 90°弯管道时的传播特性作了实验研究 ,主要是气体爆轰波通过弯管道前后的火焰速度以及加速情况的研究 ,初步得出 ,爆轰波经过弯管道后单位距离上的火焰速度增量显著增加。这一研究结果证明 ,弯曲管道对于爆燃与爆轰波火焰有明显的加速作用     

T型管道不同封闭状态瓦斯爆燃火焰传播特征

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。     

温度梯度影响爆燃转爆轰的数值模拟

采用一维带真实化学反应的Navier-Stokes方程对温度梯度影响爆燃转爆轰的过程进行了数值模拟.结果表明,点火温度的不均匀性对可燃预混气的燃烧模式有显著影响.在零温度梯度条件下,点火初期呈可燃气等容爆炸现象,随后发展为火焰传播;在小温度梯度下,点火后会导致爆轰形成,但很快衰减为爆燃过程;当温度梯度增加到合适值时,点火燃烧后可形成过驱爆轰并最终称为稳定爆轰状态;而温度梯度过大时,仅呈现正常火焰传播状态.不同温度梯度可以导致燃烧化学反应放热与热传导之间的竞争,因而形成了不同的燃烧模式.上述研究对实际过程中爆轰形成现象的防治有着一定的理论意义.     

惰性气体抑制瓦斯爆燃火焰传播特性实验研究*

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。     

温度梯度影响爆燃转爆轰的数值模拟

采用一维带真实化学反应的Navier-Stokes方程对温度梯度影响爆燃转爆轰的过程进行了数值模拟。结果表明，点火温度的不均匀性对可燃预混气的燃烧模式有显著影响。在零温度梯度条件下，点火初期呈可燃气等容爆炸现象，随后发展为火焰传播；在小温度梯度下，点火后会导致爆轰形成，但很快衰减为爆燃过程；当温度梯度增加到合适值时，点火燃烧后可形成过驱爆轰并最终称为稳定爆轰状态；而温度梯度过大时，仅呈现正常火焰传播状态。不同温度梯度可以导致燃烧化学反应放热与热传导之间的竞争，因而形成了不同的燃烧模式。上述研究对实际过程中爆轰形成现象的防治有着一定的理论意义。     

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。     

气体爆轰波在管道中绕射和反射的实验研究

本文实验研究了氢/氧/氩气体爆轰波在矩形管中900尖角绕射时的传播特性,利用烟迹技术记录了实验现象,运用爆轰波波阵面结构理论和激波绕射及反射理论对实验结果作了分析。结果表明平面气体爆轰波在900尖角绕射时由于横波失去碰撞以及稀疏波作用,稳定三波结构在绕射区发生变化,在反射激波作用下形成热点产生子爆炸,重新在垂直分支管中形成稳定爆轰波。     

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。     

泡沫金属对甲烷/空气爆燃火焰的淬熄实验研究

为研究多孔材料对甲烷/空气预混气体爆燃火焰的抑制淬熄效果,运用一套自主设计的管道爆炸抑制系统进行实验研究。在实验中运用高速摄像机记录爆燃火焰在穿过多孔材料板时的淬熄过程,采用20,40,60,80PPI (孔目数) 的4种多孔材料,研究不同孔目数的多孔材料对爆燃火焰传播的形态结构、火焰传播速度以及抑制淬熄等特性的影响。结果表明:多孔材料的孔目数对爆燃火焰传播的早期阶段影响较小,爆燃火焰都经历了半球形火焰和指形火焰阶段;当火焰传播到多孔材料板时,孔目数越大对火焰的降速作用越强,80PPI工况下爆燃火焰不能穿过多孔材料板,即发生淬熄。实验结果揭示了多孔材料对火焰的淬熄作用与微孔通道和火焰的相互作用有关。     

气体爆燃火焰在狭缝中的淬熄

通过叙述可燃气体爆燃火焰在平行板狭缝中传播时产生淬熄的实验和理论研究结果，给出了甲烷，丙烷，乙炔，氢气等四种可燃气体与空气的预混气作为实验介质所进行的爆火焰淬熄实验中，火焰传播速度与淬熄直径、淬熄长度之间的关系。对于气体爆燃火争的淬熄理论模型进行了探讨，得到了有应用价值的结论。     

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.     

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.     

无起爆药雷管内管装药密度对燃烧转爆轰的影响研究

起爆药雷管生产中产生大量有毒废水,且其运输、贮存存在安全隐患。为克服这些困难,笔者自行制备无起爆药雷管。采用圆筒式金属内管中装填超细PETN(季戊四醇四硝酸酯),作为起爆元件,代替起爆药部分,研究装药密度对内管燃烧转爆轰(DDT)的影响。研究结果表明,在内管壁厚1～2 mm,内径Φ4.0 mm,长25 mm,装压密度为0.8～1.14 g/cm3的范围内,内管能可靠实现燃烧转爆轰。     

Detonation characteristics of ammonium nitrate and activated carbon mixtures

To better understand the detonation characteristics of ammonium nitrate (AN) and activated carbon (AC) mixtures, steel tube tests were carried out for AN/AC mixtures of various compositions and different forms of AN (powdered, prilled, phase stabilized and granular), and the detonation velocity was measured. The powdered AN/AC mixtures gave higher detonation velocities than the other AN forms. For all the AN/AC mixtures, the experimentally observed detonation velocities at each loading density were far below the theoretically predicted values calculated by the CHEETAH code based on thermohydrodynamics, exhibiting so-called non-ideal detonation. The lowest detonation velocity of powdered AN/AC mixtures was obtained as D=1.25 km/s for an AC content of 0.1 wt%. This was considered to be close to the critical condition for stable detonation.     

Propagation Characteristics of Gas Explosion in Linked Vessels Based on DDT Criteria

To study the occurrence conditions and propagation characteristics of deflagration to detonation transition (DDT) in linked vessels, two typical linked vessels were investigated in this study. The DDT of the methane–air mixture under different pipe lengths and inner diameters was studied. Results showed that the CJ detonation pressure of the methane–air mixture was 1.86 MPa, and the CJ detonation velocity was 1987.4 m/s. Compared with a single pipe, the induced distance of DDT is relatively short in the linked vessels. With the increase in pipeline length, DDT is more likely to occur. Under the same pipe diameter, the DDT induction distance in the vessel–pipe–vessel structure is shorter than that in the vessel–pipe structure. With the increase in pipeline diameter, the length of the pipe required to form the DDT is reduced. For linked vessels in which detonation formed, four stages, namely, slow combustion, deflagration, deflagration to detonation, and stable detonation, occurred in the vessels. Moreover, for a pipe diameter of 60 mm and a length of 8 m, overdriven detonation occurred in the vessel–pipe–vessel structure.     

燃烧、爆炸过程复杂性行为的非线性动力学(Ⅰ)

从非线性动力学观点,总结了燃烧和爆炸系统的多种复杂现象。指出了其非线性现象之间的对应关系。提出了从非线性即从“系统”、“全局或大范围”、“演化”及“统一”地观点认识燃烧和爆炸现象的观点。     

Deflagration to detonation transition in a vapour cloud explosion in open but congested space: Large scale test

The paper reviews large scale experiments with various fuels in air where successful deflagration to detonation transition (DDT) took place. This includes a recent experiment disclosed in the Buncefield R&D program, where DDT developed in the propane/air mixture. The DDT occurred in branches of deciduous trees in a premixed stagnant mixture. An internal R&D investigation programme was initiated to better understand the phenomena. A large scale experiment in an open space with ethane air mixture is presented in the paper. The premixed mixture was ignited at the edge of the congested three-dimensional rigs which consisted of vertical and horizontal pipes. After ignition, the flame accelerated in the congestion and transitioned to detonation at the end of congestion. Stable detonation propagated through the remaining open and uncongested space.The flame acceleration process leading to DDT is scale dependent. It also depends on many parameters leading to a large investigation array and, significant cost. However, such R&D efforts aimed toward a safer plant design, i.e. the prevention of occurrence of a major accident, are a small fraction of a real accident cost.     

A violent,episodic vapour cloud explosion assessment: Deflagration-to-detonation transition

A large vapour cloud explosion (VCE) followed by a fire is one of the most dangerous and high consequence events that can occur in petrochemical facilities. The current process of safety practice in the industry in VCE assessment is to assume that all VCEs are deflagration. This assumption has been considered for nearly three decades. In recent years, major fire and VCE incidents in fuel storage depots gained considerable attention in extreme high explosion overpressure due to the transition from Deflagration to Detonation (DDT). Though the possibility of DDTs is lower than deflagrations, they have been identified in some of the most recent large-scale VCE incidents, including Buncefield (UK), 2005, San Juan explosion (US), 2009, and IOCL Jaipur (India), 2009 event. Such an incident established the need to understand not only VCE but also the importance of avoiding the escalation of minor incidents into much more devastating consequences.Despite decades of research, understanding of the fundamental physical mechanisms and governing factors of deflagration-to detonation transition (DDT) transition remains mostly elusive. An extreme multi-scale, multi-physics nature of this process uncertainly makes DDT one of the “Grand Challenge” problems of typical physics, and any significant developments toward its assured insistence would require revolutionary step forward in experiments, theory, and numerical modelling. Under certain circumstances, nevertheless, it is possible for DDT to occur, and this can be followed by a propagating detonation that quickly consumes the remaining detonable cloud. In a detonable cloud, a detonation creates the worst accident that can happen. Because detonation overpressures are much higher than those in a deflagration and continue through the entire detonable cloud, the damage from a DDT event is more severe. The consideration of detonation in hazard and risk assessment would identify new escalation potentials and recognize critical buildings impacted. This knowledge will allow more effective management of this hazard.The main conclusion from this paper is that detonations did occur in Jaipur accident at least part of the VCE accidents. The vapour cloud explosion could not have been caused by a deflagration alone, given the widespread occurrence of high overpressures and directional indicators in open uncongested areas containing the cloud. Additionally, the major incident has left many safety issues behind, which must be repeatedly addressed. It reveals that adequate safety measures were either underestimated or not accounted for seriously. This article highlights the aftermath of the IOCL Jaipur incident and addresses challenges put forward by it.     

管道中氢气-空气爆轰的多级泄爆数值模拟研究

为了研究管道内氢气的爆燃转爆轰及其抑制过程,对单个障碍物管道中氢气-空气混合物燃爆过程以及多级泄爆进行了二维数值模拟。基于氢气-空气19步详细化学反应动力学机理,以及k-ε湍流模型、概率密度函数输运方程和同位网格SIMPLE算法,采用计算流体软件Fluent进行模拟。结果表明:密闭管道无泄爆时,在距点火端1.5 m左右爆燃转为爆轰;泄爆口的位置对管道内氢气-空气预混气体的爆炸参数有重要影响,泄爆口位于管道中部时,能降低管道内爆轰超压,泄爆效果较好;位于管道中部单个泄爆口泄爆时,有效降低爆轰超压,管道中部设置2个泄爆口时,能通过压力和混合气体的泄放将管道中已经发生的爆轰衰减为爆燃;当有3个泄爆口泄爆时,管道中没有发生爆轰,达到良好的泄爆效果。