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作 者:齐圣 杜扬[1] 梁建军[1] 张培理[1] Qi Sheng Du Yang Liang Jianjun Zhang Peili(Department of Petroleum Supply Engineering, Logistical Engineering University, Chongqing 401331, China)
机构地区:[1]后勤工程学院军事供油工程系,重庆401311
出 处:《爆炸与冲击》2016年第6期832-838,共7页Explosion and Shock Waves
基 金:国家自然科学基金项目(51276195)
摘 要:通过受限空间油气爆燃可视化实验发现,在不同初始油气体积分数下,爆燃火焰呈现出不同的表观特征,据此提出了受限空间油气爆燃的3种火焰形态,即光滑球形火焰、褶皱球形火焰和卷曲絮状火焰。分析了3种火焰形态的形成机理,并通过实验观测与理论分析,给出了区分3种火焰形态的临界条件。结合实验中采集到的关键参数,总结了不同的火焰形态下受限空间油气爆燃的反应产物、最大压力、升压速率、反应时间、火焰强度等关键参数的特征与变化规律。In order to investigate the flame characteristics of gasoline-air mixture deflagration in a confined space,visualized experiments were performed at different equivalence ratios.Three flame patterns of gasoline-air deflagration were proposed:smooth spherical flame,fold spherical flame and curling flocculent flame.Based on the chemical kinetics and flame spectroscopy,the forming mechanism of each flame pattern was examined.Then,the critical equivalence ratio,here used to distinguish the flame patterns,was obtained by theoretical analysis and experimental measurement.Combined with the collected key parameters in the experiments,the differences in key parameters of each flame pattern were summarized,such as reaction products,rate of pressure rise,flame intensity,duration of flame and maximum pressure.
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