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火焰点火器的设计
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作者 朱艳辉 高俊国 +1 位作者 张芳 张倩 《火工品》 CAS CSCD 北大核心 2006年第4期22-25,共4页
针对焊接药剂的特点,并结合焊条的具体结构,采用专用火焰点火器点燃焊条的设计方案,并对点火器进行了详细设计。针对点火能量需求,确定了以硅粉、硝酸钡和硫磺为主要组分的高能点火药配方,同时围绕点火器安全性、可靠性、贮存性能等方... 针对焊接药剂的特点,并结合焊条的具体结构,采用专用火焰点火器点燃焊条的设计方案,并对点火器进行了详细设计。针对点火能量需求,确定了以硅粉、硝酸钡和硫磺为主要组分的高能点火药配方,同时围绕点火器安全性、可靠性、贮存性能等方面进行了多项性能试验,最终证实该点火器能够满足焊接设备的正常使用需求。 展开更多
关键词 火焰点火 焊接 点火
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预燃室火焰射流点火对汽油机性能影响的研究 被引量:3
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作者 陈泓 李钰怀 +3 位作者 罗亨波 杜家坤 江枭枭 王磊 《内燃机工程》 EI CAS CSCD 北大核心 2021年第3期61-66,73,共7页
在一款增压直喷小型强化废气涡轮增压汽油机上,进行了加装预燃室与传统点火在低速外特性、中转速负荷特性的燃烧特性、经济性和排放特性对比试验,分析了预燃室火焰射流点火过程与传统点火对汽油机性能影响的规律。研究结果表明,在1500 r... 在一款增压直喷小型强化废气涡轮增压汽油机上,进行了加装预燃室与传统点火在低速外特性、中转速负荷特性的燃烧特性、经济性和排放特性对比试验,分析了预燃室火焰射流点火过程与传统点火对汽油机性能影响的规律。研究结果表明,在1500 r/min、平均有效压力为2 MPa工况,采用预燃室点火后缸内燃烧等容度提高,最高燃烧压力增大,燃烧相位提前7.1°,有效燃油消耗率下降约24 g/(kW·h);在2000 r/min负荷特性的试验工况,相比于传统点火,预燃室点火燃烧循环变动均获得改善,燃烧持续期缩短,低负荷时燃烧相位不变而比油耗略微上升,高负荷时燃烧相位大幅提前,比油耗改善约7 g/(kW·h),且最高有效热效率由36.9%上升至37.5%。就气体排放物而言,预燃室点火加速燃烧使NO x排放最高上升约15%,HC排放最多下降约36%,而CO排放低负荷时基本维持不变,在高负荷时略有下降。 展开更多
关键词 预燃室 火焰射流点火 汽油机 性能 排放
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一种抗高过载高离心旋转的全密封火焰延期点火管 被引量:1
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作者 蔺美君 贾宁科 +3 位作者 刘海旭 杨正才 陈雨 王敏 《火工品》 CAS CSCD 北大核心 2018年第5期1-4,共4页
为了研制一种既能抗径向高过载的冲击,又能满足高离心旋转条件下延期精度的全密封火焰延期点火管,进行了闭气机构设计及试验验证。研究表明:采用组合化单孔传火垫片设计,解决了延期点火管径向抗高过载冲击的问题;采用闭气机构设计,提高... 为了研制一种既能抗径向高过载的冲击,又能满足高离心旋转条件下延期精度的全密封火焰延期点火管,进行了闭气机构设计及试验验证。研究表明:采用组合化单孔传火垫片设计,解决了延期点火管径向抗高过载冲击的问题;采用闭气机构设计,提高了延期点火管在高离心过载条件下的延期精度和输出性能稳定性。在系统试验中,该延期点火管均可靠作用。 展开更多
关键词 火焰延期点火 延期精度 高过载 闭气机构 单孔传火垫片
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液体亚燃燃烧室点火装置工作特性数值研究 被引量:1
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作者 陈博 林木 +1 位作者 吴宝元 刘志让 《火箭推进》 CAS 2013年第6期6-11,共6页
基于气体动力学和计算流体力学的相关理论,采用CFD-ACE+流场计算软件,对液体亚燃燃烧室点火装置单独工作时的稳态流场进行了数值模拟。在试验验证的基础上分析了点火器室压、点火导管内径和导管的结构形式对火焰点火性能的影响。结果表... 基于气体动力学和计算流体力学的相关理论,采用CFD-ACE+流场计算软件,对液体亚燃燃烧室点火装置单独工作时的稳态流场进行了数值模拟。在试验验证的基础上分析了点火器室压、点火导管内径和导管的结构形式对火焰点火性能的影响。结果表明:当点火器室温和燃气流量恒定时,若保持管道的扩张比不变,选用较低室压的点火器更利于点火;在一定范围内增大导管内径可以提高火焰的点火性能;燃气在直管内的流动损失较小,出口射流的速度较高,穿透深度较大,带弯头的点火导管出口火焰特征类似,有无弯头对火焰的影响很大,而角度差异产生的影响很小。 展开更多
关键词 液体亚燃燃烧室 点火装置 火焰点火性能 稳态流场 数值模拟
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脉冲爆震发动机新型点火系统的优化设计 被引量:1
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作者 姜日红 武晓松 +1 位作者 余陵 陈志刚 《南京理工大学学报》 EI CAS CSCD 北大核心 2009年第2期225-229,共5页
为了缩短爆燃向爆震转捩的时间和距离,该文将一种新型点火系统——火焰喷射点火系统应用于脉冲爆震发动机。利用二维数值模拟研究不同喷射点火系统结构参数(前端圆柱段长度,直径以及末端喷嘴的直径)下爆燃向爆震转捩的时间和距离,并将... 为了缩短爆燃向爆震转捩的时间和距离,该文将一种新型点火系统——火焰喷射点火系统应用于脉冲爆震发动机。利用二维数值模拟研究不同喷射点火系统结构参数(前端圆柱段长度,直径以及末端喷嘴的直径)下爆燃向爆震转捩的时间和距离,并将研究结果与传统点火系统的爆燃向爆震转捩转变时间进行对比。结果发现:对于该文所采用的PDE模型,最有效的副室结构为喷嘴直径4 mm,副室长度10 mm,体积3.8 cm3。此外还发现喷射点火系统比传统点火系统能更有效地缩短爆燃向爆震转捩的时间和距离,其效率约为后者的1.26倍。 展开更多
关键词 脉冲爆震发动机 火焰喷射点火系统 爆燃向爆震转捩 传统点火系统 二维数值模拟
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一堂别开生面的化学实验课
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作者 李国忠 《潍坊工程职业学院学报》 1988年第S1期75-77,共3页
今学期我们利用课外活动时间上了一堂别开生面的化学实验课一由课外学习小组的同学自已设计,自己组装,自己向全体同学表演了改进后的一氧化碳还原氧化铜的实验,引起了同学们极大的学习兴趣,取得了意想不到的良好效果.
关键词 化学实验课 课外学习 初中化学 集气瓶 接触时间 气体还原剂 启发诱导 第斯多惠 浅蓝色 火焰点火
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Methane–air explosion characteristics with different obstacle configurations 被引量:17
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作者 Wen Xiaoping Yu Minggao +2 位作者 Ji Wentao Yue Meng Chen Junjie 《International Journal of Mining Science and Technology》 SCIE EI CSCD 2015年第2期213-218,共6页
To investigate the flame and overpressure characteristics of methane–air explosion with different obstacle configurations,an experimental study has been conducted,taking account of the number of obstacles,obstacle di... To investigate the flame and overpressure characteristics of methane–air explosion with different obstacle configurations,an experimental study has been conducted,taking account of the number of obstacles,obstacle distance from ignition source,and stream-wise and cross-wise obstacle positions.The results show that the flame speed and peak overpressure increase with the increasing number of obstacles,while the time to reach the peak is not fully determined by it.And the configuration having the farthest obstacle produces a higher overpressure and takes a longer time to reach the peak,but a slower flame propagation speed is obtained.Similar explosion characteristics are also observed in the configurations with two obstacles fixed at different stream-wise positions.Furthermore,the experimental results demonstrate that the peak overpressures and flame speeds in configurations with central or staggered obstacles are relatively higher,which should to be avoided in practical processes to minimize the risk associated with methane–air explosion. 展开更多
关键词 Methane-air explosion Obstacle configurations Flame propagation Overpressure
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工业炉燃烧系统应用技术探讨 被引量:3
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作者 刘小静 余志华 《工业加热》 CAS 2003年第3期33-36,共4页
燃烧及其控制技术是各种火焰炉技术核心,强调高水平燃烧系统应对燃烧全过程进行控制,着重对燃烧系统点火、火焰监测、空燃比比例调节、燃烧过程各参数监控、炉温自动控制等各个方面内容进行了讨论介绍,最后用某天然气加热炉燃烧系统原... 燃烧及其控制技术是各种火焰炉技术核心,强调高水平燃烧系统应对燃烧全过程进行控制,着重对燃烧系统点火、火焰监测、空燃比比例调节、燃烧过程各参数监控、炉温自动控制等各个方面内容进行了讨论介绍,最后用某天然气加热炉燃烧系统原理图及应用效果进行实例说明。 展开更多
关键词 燃烧系统 点火火焰监测 空燃比 比例调节
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Experimental and numerical evaluations on characteristics of vented methane explosion 被引量:2
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作者 SU Bin LUO Zhen-min +1 位作者 WANG Tao LIU Lang 《Journal of Central South University》 SCIE EI CAS CSCD 2020年第8期2382-2393,共12页
To research the characteristics of vented explosion of methane-air mixture in the pipeline,coal mine tunnel or other closed space,the experiments and numerical simulations were carried out.In this work,explosion chara... To research the characteristics of vented explosion of methane-air mixture in the pipeline,coal mine tunnel or other closed space,the experiments and numerical simulations were carried out.In this work,explosion characteristics and flame propagation characteristics of methane in pipeline and coal mine tunnel are studied by using an explosion test system,combined with FLACS software,under different vented conditions.The numerical simulation results of methane explosion are basically consistent with the physical experiment results,which indicates that the numerical simulation for methane explosion is reliable to be applied to the practice.The results show that explosion parameters(pressure,temperature and product concentration)of methane at five volume fractions have the same change trend.Nevertheless,the explosion intension of 10.0%methane is the largest and that of 9.5%methane is relatively weak,followed by 11.0%methane,8.0%methane and 7.0%methane respectively.Under different vented conditions,the pressure and temperature of methane explosion are the highest in the pipeline without a vent,followed by the pipeline where ignition or vent position is in each end,and those are the lowest in the pipeline with ignition and vent at the same end.There is no significant effect on final product concentration of methane explosion under three vented conditions.For coal mine tunnel,it is indicated that the maximum explosion pressure at the airproof wall in return airway with the branch roadway at 50 m from goaf is significantly decreased while that in intake airway does not change overwhelmingly.In addition,when the branch roadway is longer or its section is larger,the peak pressure of airproof wall reduces slightly. 展开更多
关键词 methane-air flame propagation CFD simulation vented explosion ignition position peak pressure
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CO_(2)-diluted CH_(4)-air premixed spherical flames with microwave-assisted spark ignition
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作者 ZHANG Xin-hua WANG Zhao-wen +5 位作者 WU Hui-min LIU Chao-hui WANG Zhi-hao LI Xiao-jie CHENG Xiao-bei CHEN Jyh-Yuan 《Journal of Central South University》 SCIE EI CAS CSCD 2022年第7期2157-2164,共8页
The performance of microwave-assisted spark ignition(MAI)under exhaust gas recirculation conditions was explored with CO_(2)-diluted CH-air premixed spherical flames in a constant volume combustion chamber.The flame k... The performance of microwave-assisted spark ignition(MAI)under exhaust gas recirculation conditions was explored with CO_(2)-diluted CH-air premixed spherical flames in a constant volume combustion chamber.The flame kernel radius at 5 ms after spark started was selected to evaluate the property of MAI for CO_(2)dilution ratio of 0-20%and equivalence ratio of 0.6-1.4 with 1 kHz microwave pulse repetition frequency under 0.2 MPa ambient pressure.The results showed that the addition of microwave induced some wrinkles on the flame surface and strongly deformed the flame.MAI expanded the limit of CO_(2)dilution ratio to 16%with an equivalence ratio of 0.75,in which case the spark only(SI)failed to ignite the mixture.With the CO_(2)dilution ratio increasing,the wrinkles induced by microwave pulses decreased apparently,and the enhancement value of MAI peaked at 4%CO_(2)dilution ratio.The effect of microwave was considered in two aspects,namely,reaction kinetics and thermal effect,which shows a“trade-off”as CO_(2)dilution ratio rose.With 8%volume of CO_(2)added,the flammable interval(equivalence ratio 0.6-1.2)of mixture in SI mode shrunk,and MAI can maintain a flammable interval consistency with the case that no CO_(2)was added. 展开更多
关键词 microwave spark ignition CO_(2)dilution spherical flame flame surface wrinkles
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Simulation of Turbulent Combustion Flame Feature Based on Fractal Theory for SI Engines
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作者 张军 杜青 +1 位作者 宋东先 杨延相 《Transactions of Tianjin University》 EI CAS 2010年第4期256-261,共6页
The flame structure of gasoline engine is complicated and has the characteristic of fractal geometry. A fractal combustion model was used to simulate the engine working cycle. Based on this model, the fractal dimensio... The flame structure of gasoline engine is complicated and has the characteristic of fractal geometry. A fractal combustion model was used to simulate the engine working cycle. Based on this model, the fractal dimension and laminar flame surface area of turbulent premixed flames were studied under different working conditions. The experimental system mainly includes an optical engine and a set of photography equipment used to shoot the images of turbulent flame of spark-ignition engine. The difference box-counting method was used to process 2D combustion images. In contrast to the experimental results, the computational results show that the fractal combustion model is an effective method of simulating the engine combustion process. The study provides a better understanding for flame structure and its propagation. 展开更多
关键词 turbulent combustiom fractal SIMULATION optical engine
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子母火箭中子火箭的点火
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作者 李树军 《轻兵器》 1999年第11期25-26,共2页
前言 自60年代武装直升机问世以来,便以其独特的攻击能力、作战机动性和超强的生存能力日益受到世界许多国家的重视并得到迅速发展。目前,随着武装直升机装备数量的增加,战斗性能的加强,对战场上步兵、炮兵、装甲兵及后勤保障系统的威... 前言 自60年代武装直升机问世以来,便以其独特的攻击能力、作战机动性和超强的生存能力日益受到世界许多国家的重视并得到迅速发展。目前,随着武装直升机装备数量的增加,战斗性能的加强,对战场上步兵、炮兵、装甲兵及后勤保障系统的威胁也愈来愈大。为了有效地保护自己,消灭敌人,争取战场上的主动权,各国在大力发展武装直升机的同时。 展开更多
关键词 武装直升机 火箭点火 传火药 推进剂 火焰点火 中子 延期药 后勤保障系统 子母 战斗部
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几则初中化学演示实验的延伸设计
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作者 钱国山 《中学化学教学参考》 2014年第3X期54-54,共1页
正反两个方面的经验,才是完善的经验。"吃一堑长一智""失败乃成功之母",都说明了这个道理。因此,在化学实验教学中,我们不应回避实际的反面操作及其现象,只是纸上谈兵,相反,应该适时和安全地延伸实验操作,尽力"... 正反两个方面的经验,才是完善的经验。"吃一堑长一智""失败乃成功之母",都说明了这个道理。因此,在化学实验教学中,我们不应回避实际的反面操作及其现象,只是纸上谈兵,相反,应该适时和安全地延伸实验操作,尽力"放大"反面操作及其现象,并引导学生观察体验和深入地思考,使他们获得全面的感性认识、深刻的理性认识,从而扎实提高课堂的教学效率。以下是本人对于人教版九年级化学教科书中的几则演示实验的延伸设计,仅供参考。一、实验2-5"加热高锰酸钾制取氧气(图2-14)"演示排水法收集氧气完毕,是先从水槽中取出导管。 展开更多
关键词 化学教科书 初中化学 排水法 人教版 橡皮塞 爆鸣 火焰点火 气体压强 饮料瓶 可燃性气体
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Ignition, flame propagation and extinction in the supersonic mixing layer flow 被引量:7
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作者 ZHANG YunLong WANG Bing ZHANG HuiQiang 《Science China(Technological Sciences)》 SCIE EI CAS 2014年第11期2256-2264,共9页
The supersonic mixing layer flow,consisting of a relatively cold,slow diluted hydrogen stream and a hot,faster air stream,is numerically simulated with detailed transport properties and chemical reaction mechanisms.Th... The supersonic mixing layer flow,consisting of a relatively cold,slow diluted hydrogen stream and a hot,faster air stream,is numerically simulated with detailed transport properties and chemical reaction mechanisms.The evolution of the combustion process in the supersonic reacting mixing layer is observed and unsteady phenomena of ignition,flame propagation and extinction are successfully captured.The ignition usually takes place at the air stream side of braid regions between two vortexes due to much higher temperature of premixed gases.After ignition,the flame propagates towards two vortexes respectively located on the upstream and downstream of the ignition position.The apparent flame speed is 1569.97 m/s,which is much higher than the laminar flame speed,resulting from the effects of expansion,turbulence,vortex stretching and consecutive ignition.After the flame arrives at the former vortex,the flame propagates along the outer region of the vortex in two branches.Then the upper flame branch close to fuel streamside distinguishes gradually due to too fuel-riched premixed mixtures in the front of the flame and the strong cooling effect of the adjacent cool fuel flow,while the lower flame branch continues to propagate in the vortex. 展开更多
关键词 supersonic mixing layer IGNITION flame propagation EXTINCTION
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Experimental Study on Spark Ignition of Non-premixed Hydrogen Jets 被引量:1
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作者 Jin Guo Changjian Wang +1 位作者 Manhou Li Qize He 《Journal of Thermal Science》 SCIE EI CAS CSCD 2014年第4期354-358,共5页
The leaks of pressurized hydrogen can be ignited if an ignition source is within a certain distance from the source of the leaks, and jet ftres or explosions may take place. In this paper, a high speed camera was used... The leaks of pressurized hydrogen can be ignited if an ignition source is within a certain distance from the source of the leaks, and jet ftres or explosions may take place. In this paper, a high speed camera was used to investigate the ignition kernel development, ignition probability and flame propagation along the axis of hydrogen jets, which leaked from a 3-ram-internal-diameter nozzle and were ignited by an electric spark. Experimental results indicate that for successful ignition events, the ignition delay time increases with an increase of the distance between the nozzle and the electrode. Ignitable zone of the hydrogen jets is underestimated if using the predicted hydrogen concentration along the jets centerline. The average rate of downstream flame decreases but that of the upstream flame increases with the electrode going far from the nozzle. 展开更多
关键词 HYDROGEN Spark ignition Ignition kernel Ignition probability Flame propagation
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