安全帽质量低劣8元一顶 成为施工人员的遮阳帽

按照国家标准,一顶合格安全帽的承重为5千克,可经受从1米高处下落造成的冲击6月7日,媒体报道了"钢筋从天而降直接插进工人头部"一事,安全帽质量问题引起了人们的关注。市场上的安全帽合格吗?意外发生时安全帽能起到防护作用吗?就此,记     

安全帽质量低劣8元一顶成为施工人员的遮阳帽

按照国家标准,一顶合格安全帽的承重为5千克,可经受从1米高处下落造成的冲击 6月7日,媒体报道了"钢筋从天而降直接插进工人头部"一事,安全帽质量问题引起了人们的关注.     

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。     

工地用安全帽抽查合格率仅50％生命安危成赌博——安全帽质量低劣8元一顶 成为施工人员的遮阳帽

按照国家标准,一顶合格安全帽的承重为5千克,可经受从1米高处下落造成的冲击6月7日,媒体报道了＂钢筋从天而降直接插进工人头部＂一事,安全帽质量问题引起了人们的关注。市场上的安全帽合格吗？意外发生时安全帽能起到防护作用吗？就此,     

水雾抑制气体爆炸火焰传播的实验研究

利用自行设计的全程透明的火焰加速管系统和细水雾实验系统 ,对不同水雾条件下的气体火焰传播现象进行了实验研究。运用光电传感器与CCD摄像技术 ,笔者分析了不同水雾条件下的甲烷预混气体火焰传播速度、传播火焰阵面轨迹 ;探讨了水雾抑制气体火焰传播的机理及条件。实验发现了在一定条件水雾作用下的气体传播火焰阵面拉伸与火焰驻留的现象与条件 ,实验结果表明 :水雾对气体爆炸火焰传播的抑制是由于水雾作用于火焰阵面反应区 ,降低了反应区内火焰温度和气体燃烧速度 ,减缓了火焰阵面传热与传质的进行 ,从而使传播火焰得以抑制 ;而水雾对气体爆炸火焰传播的抑制效果与水雾通量、雾区浓度、水雾区长度以及火焰到达水雾区的火焰传播速度有关     

国内外安全帽标准探讨与研究

本文通过对欧美国家新旧安全帽标准之系统对比与研究,并经过不同标准的安全帽性能的差异化测试,取得了一些实验检测数据。建议安全帽国家标准重新修订时,适应时代需求,以求取长补短,制定与完善部分安全性能条款,进一步保护劳动者的头部安全。     

多孔材料对管道内甲烷-空气预混火焰传播的影响

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。     

柱形连通容器内预混气体爆炸过程的火焰传播模拟

为研究连通容器内气体爆炸规律,采用Fluent(经典流体动力学软件)对柱形连通容器内预混气体爆炸过程进行模拟,模拟了不同点火位置和火焰传播方向条件下连通容器内火焰传播过程和压力变化,并分析了连通容器内不同时刻的速度场.结果表明:火焰面在传播过程中并非完全对称,当火焰到达传爆容器后,湍流燃烧剧烈,火焰不规则变形显著;端面点火后在传爆容器内产生的压力峰值和压力波动比中心点火时更大;当起爆容器为大容器时,传爆容器内气体预压缩程度更大,压力峰值更高.     

水雾作用下气体爆炸火焰传播的实验研究

利用自行设计的全程透明的火焰加速管和水喷雾系统，对不同水雾条件下的气体火焰传播现象进行了实验研究。运用光电传感器与数字摄像技术分析了不同浓度的甲烷在不同水雾条件下的火焰传播速度、火焰阵面轨迹以及火焰结构特性，并通过对传播火焰反应区温度的测量，探讨了水雾抑制气体爆炸火焰传播的内在机理及所需的条件。实验结果表明：由于水雾作用于火焰反应区，降低了火焰反应区内的温度和气体燃烧速度，延长火焰阵面的预热区，减缓火焰阵面传热与传质的进行，从而使传播火焰得以抑制。水雾对气体爆炸火焰传播的抑制效果与水雾流量速度、雾区浓度以及火焰到达水雾区的火焰传播速度有关。     

管道结构对氢/空预混气体爆炸特性影响研究

为研究管道结构对氢-空预混气体爆炸特性影响,采用实验与数值模拟相结合的方法,分析不同管道结构内氢-空预混气体燃爆时火焰传播进程、爆炸压力、湍流动能变化及流场分布.结果表明:90°弯管对氢-空预混气体爆炸强度增强作用明显高于T型分岔管和直管.火焰阵面在结构突变处褶皱变形较明显,并出现大尺度强湍流和涡团,气团脉动速度与湍流...     

A new laboratory rig for evaluating helmets subject to oblique impacts

Current requirements and regulations governing motorcycle helmets around the world are based on test results of purely radial impacts, which are statistically rare in real accidents. This study presents a new impact rig for subjecting test helmets to oblique impacts, which therefore is able to test impacts of increased statistical relevance to real motorcycle accidents. A number of different head-helmet interfaces have been investigated. A test rig was constructed to produce oblique impacts to helmets simulating those occurring in real motorcycle accidents. A Hybrid III dummy head was fitted with accelerometers to measure the accelerations arising during impact testing. The equipment used for data collection was validated in both translational and rotational acceleration. In order to better resemble the human head, an artificial scalp was fitted to the hybrid dummy. The same test rig was used to investigate the performance of a number of different helmets. Impact velocities ranging from 7.3 to 9.9 m/s were tested using a number of different impact angles and impact areas. This study shows that the new test rig can be used to provide useful data at speeds of up to 50 km/h and with impact angles varying from purely tangential to purely radial. The rotational accelerations observed differ greatly depending on both helmet and scalp designs. For example, a helmet with a sliding outer shell placed on an experimental head fitted with an artificial scalp (made to resemble the human scalp) reduces rotational accelerations of the head by up to 56%, compared with those of an experimental head fitted with a fixed scalp and conventional helmet. The degree of slippage between the skull and the scalp, and between the scalp and the helmet, leads to considerable variation in the results. This innovative test rig appears to provide an accurate method for measuring accelerations in an oblique impact to a helmet. In order to obtain a good level of repeatability in oblique impact testing, it is crucial that the helmet be fixed to the head in the exact same way in each individual test. Both the position and the angle of impact must be reproduced identically in each test. The test rig used here has shown that this type of rig can be used to compare different helmet designs, and it therefore is able to contribute to achieving safer helmets.     

Experimental study on CO2/CF3I suppression of methane-air explosion and flame propagation

To explore the inhibitory effects of CF₃I and CO₂ gas on the explosion pressure and flame propagation characteristics of 9.5% methane, a spherical 20 L experimental explosion device was used to study the effect of the gas explosion suppressants on the maximum explosion pressure, maximum explosion pressure rise rate and flame propagation speed of methane. The results indicated that with a gradual increase in the volume fraction of the gas explosion suppressant, the maximum explosion pressure of methane and maximum explosion pressure rise rate gradually decreased, and the time taken to reach the maximum explosion pressure and maximum explosion pressure rise rate was gradually delayed. At the same time, the flame propagation speed gradually decreased. Additionally, the time taken for the flame to reach the edge of the window and the time taken for a crack as well as a cellular structure to appear on the flame surface was gradually delayed. The fluid dynamics uncertainty was suppressed. The explosion pressure and flame propagation processes were markedly suppressed, but the flame buoyancy instability was gradually enhanced. By comparing the effects of the two gas explosion suppressants on the pressure and flame propagation characteristics, it was found that at the same volume fraction, trifluoroiodomethane was significantly better than carbon dioxide in suppressing the explosion of methane. By comparing the reduction rates of the characteristic methane explosion parameters at a volume fraction of 9.5%, it was observed that the inhibitory effect of 4% trifluoroiodomethane on the maximum explosion pressure was approximately 4.6 times that of the same amount of carbon dioxide, and the inhibitory effect of 4% trifluoroiodomethane on the maximum explosion pressure rise rate and flame propagation speed was approximately 2.7 times that of the same amount of carbon dioxide. The addition of 0.5%–1.5% trifluoromethane to 4% and 8% carbon dioxide can improve the explosion suppression efficiency of carbon dioxide. This enhancing phenomenon is a comprehensive manifestation of the oxygen-decreasing effect of carbon dioxide and the trifluoroiodomethane-related endothermic effect and reduction in key free radicals.     

瓦斯爆炸阻隔爆装置失效原因的实验研究

通过对水平管道内瓦斯爆炸的火焰结构及压力结构的实验研究 ,分析了瓦斯爆炸阻隔爆装置的失效原因。结果表明 ,瓦斯爆炸火焰是沿着管道的底部向前传播的 ,火焰长度较长 ,并具有较高的内聚力。阻隔爆装置的失效原因是由于其动作延迟时间与火焰到达装置位置所需的时间不一致 ,使释放出的抑制剂不能有效地覆盖整个火焰区 ,造成具有较高内聚力的火焰 ,在其后部巨大爆炸产物膨胀压力的推动下继续向前传播     

对称障碍物条件下瓦斯爆炸火焰与压力波耦合作用研究

为了研究对称障碍物条件下瓦斯爆炸压力波与火焰传播的耦合作用,在150 mm×150 mm×1 700 mm的有机玻璃瓦斯爆炸管道中,距离点火端不同距离安装0.5阻塞率的对称障碍物,进行8.5%甲烷体积分数的爆炸试验,采集瓦斯爆炸的超压信号并同步拍摄火焰传播图像。结果表明:火焰穿越板式对称障碍物的过程经历了火焰加速、火焰降速到火焰再加速的过程,火焰降速的时间仅为5 ms。距离点火焰源不同长度的对称障碍物在火焰加速过程中的作用存在明显差异,近点火源的障碍物作用主要为诱导湍流,远离点火源的障碍物作用主要为湍流增强。     

连通容器气体密闭爆炸与泄爆过程的实验研究

利用球型容器与管道组合,开展连通容器气体爆炸与泄爆实验,分析连通条件下,火焰在管道中的传播过程及其对起爆容器和传爆容器的压力影响。实验结果表明:连通容器气体爆炸中,火焰从起爆容器到传爆容器传播经历了一段不断加速,但加速度不断减小的过程;泄爆过程中,火焰传播过程与密闭爆炸时基本一致。管道中火焰加速传播,使得传爆容器的爆炸压力和强度相较于作为起爆容器时均明显增加,危险更大,采用与起爆容器相同的泄爆面积,无法满足对连通容器中传爆容器的泄爆。同时,泄爆是一个快速的能量泄放过程应选择合理的泄爆方式,防止二次危害。     

冷冻取芯过程煤芯瓦斯解吸特性试验研究

为探究冷冻取芯过程煤芯瓦斯解吸特性,基于模拟试验的相似性,依托自主研发的含瓦斯煤冷冻取芯响应特性测试平台,开展不同变质程度煤样(长焰煤、贫瘦煤、无烟煤)及不同吸附平衡压力(1.0,2.0,3.0,4.0 MPa)下冷冻取芯过程煤芯瓦斯解吸特性试验研究。研究结果表明：冷冻取芯过程中,煤芯瓦斯解吸量与吸附平衡压力及煤变质程度呈正相关关系;在煤芯瓦斯解吸过程中存在倒吸现象,煤与瓦斯初始吸附平衡压力越大,煤的变质程度越高,倒吸开始时间越迟;冷冻取芯过程中,瓦斯解吸速度与吸附平衡压力及煤变质程度呈正相关关系,且瓦斯解吸速度随吸附平衡压力及煤变质程度变化曲线符合幂函数关系。     

障碍物压力反射特性对瓦斯爆炸传播影响的数值模拟研究*

为了研究不同形状障碍物对瓦斯爆炸传播的影响机理,对直径0.2 m、长6.5 m的密闭直管道内的瓦斯爆炸过程进行数值模拟。研究结果表明:在该实验条件下,对于火焰通过整个管道的时间,方形障碍物时间最长,球形障碍物与无障碍物时间接近,且用时最短;无障碍物时,在反射压力波作用下火焰传播速度存在明显的波动特性;有障碍物时,障碍物的诱导作用要大于反射压力波的作用,火焰传播的这种波动特性得到抑制,提升了火焰前锋向未燃区域传播的能力;压力波的波动频率与气流震荡、压力波反射叠加有关,波幅则主要与正向压力波和反射压力波的叠加效果有关。研究结果为煤矿瓦斯爆炸事故防治及隔抑爆技术应用提供技术支撑。     

不同含水率煤尘在瓦斯爆炸诱导下爆炸传播规律研究

为了探究不同含水率煤尘在瓦斯爆炸诱导下的爆炸传播规律,利用自行搭建的直管瓦斯爆炸诱导煤尘二次爆炸实验系统,从冲击波压力和火焰传播速度2个方面,研究了不同含水率沉积煤尘在瓦斯爆炸诱导下的爆炸传播规律和原因。研究结果表明:当煤尘含水率小于40%时,管道内沉积煤尘会在瓦斯爆炸诱导下产生二次爆炸,同时沉积煤尘总量一定时,沉积煤尘二次爆炸产生的冲击波超压峰值和火焰传播速度随着煤尘含水率的增加先增大后减小;当沉积煤尘含水率为20% 时,煤尘二次爆炸产生的冲击波超压峰值、火焰传播速度峰值达到最大值,分别为1.657 MPa和468.060 m/s;当沉积煤尘含水率大于40%时,沉积煤尘无法产生二次爆炸,此时爆炸产生的威力小于单一瓦斯爆炸,火焰传播速度衰减较无煤尘的瓦斯爆炸更快,沉积煤尘起到抑制瓦斯爆炸传播的作用。研究结果可以为防治煤尘二次爆炸提供理论依据。     

The influence of inert gas on limiting experimental safe gap of fuel-air mixtures at various initial pressures

The Maximum Experimental Safe Gap (MESG) is an important criterion to assess the propagation of flames through small gaps. This safety-related parameter is used to classify the flammable gases and vapors in explosion groups, which are fundamental to constructional explosion protection. It is used both, for the safe design of flameproof encapsulated devices as well as for selecting flame arresters appropriate to the individual application. The MESG of a fuel is determined experimentally according to the standard ISO/IEC 80079-20-1:2017 at normal conditions (20 °C, 1.0 bar) with air as oxidizing gas. The aim of this work is to investigate the effect of inert gas addition on the MESG in order to assess the effectiveness of inertization in constructional explosion protection. The term limiting experimental safe gap (S_G) is used for the result of these measurements. The fuel-air mixtures (fuels: hydrogen, ethylene, propene, methane) used as representatives for the explosion groups in flame arrester testing were chosen and diluted with inert gas (nitrogen, carbon dioxide) before testing. The dependence of the limiting experimental safe gap on the total initial pressure, amount and nature of inert additive is discussed. The initial pressure was varied up to 2.0 bar to include increased pressure conditions used in flame arrester testing. Apart from the well-known reciprocal dependence on the initial pressure, the added inert gas results in an exponential increase of S_G. This effect depends on the inertizing potential of the gas and is therefore different with nitrogen and carbon dioxide. The ranking of the fuels is the same as with MESG. As a result, various mixtures of the same limiting experimental safe gap can now be chosen and tested with an individual flame arrester to prove the concept of a constant and device-related limiting safe gap. The work was funded by BG-RCI in Heidelberg (PTB grant number 37056).