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IGNITION OF BINARY MIXTURE DROPLETS BY A PROPAGATING LAMINAR FLAME

机译:传播层流火焰点燃二元混合物液滴

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An experimental study was made of the ignition process of single droplets of binary mixtures subjected to a laminar flat flame propagating through a lean homogeneous propane/air mixture at constant pressure. Binary fuels consisting of n-hexane and n-hexadecane or n-dodecane, and benzene and n-hexadecane were tested. Water-emulsified liquids consisting of n-dodecane, and pure fuels like n-hexane, n-octane, n-do-decane, and n-hexadecane, were used as well. A combustion chamber made of a transparent duct was installed with spark electrodes, fine quartz fibers to suspend fuel droplets, and a shutter to allow the burned gas to escape at the top end. A high-speed video camera was provided for photographic observation of each droplet ignited by the propagating flame. The ignition delay of pure fuel droplets increased mono-tonically with increase of the initial droplet diameter and decrease of fuel volatility. The influence of the initial droplet diameter on the ignition delay decreased with increasing fuel volatility. Ignition delay of the binary fuel droplets decreased with an increase of the volume concentration of the higher-volatility fuel. Ignition delay of the binary fuels showed a minimum and a maximum as a function of the initial droplet diameter. The diameters at the minimum and the maximum of ignition delay decreased with increasing higher-volatility fuel concentration. For the emulsified fuel, on the other hand, ignition delay increased with increasing initial droplet diameter and increasing water content. Part of the propagating flame behind the droplet became convex toward the unbumed gas as it passed a droplet of higher-volatility fuels, while the flame remained flat for the lower-volatility fuels. The deformation length of the propagating flame behind the droplet increased with increasing higher-volatility fuel concentration.
机译:对二元混合物的单滴的点火过程进行了实验研究,该混合物经受层状扁平火焰并在恒定压力下通过稀薄的均相丙烷/空气混合物传播。测试了由正己烷和正十六烷或正十二烷以及苯和正十六烷组成的二元燃料。还使用了由正十二烷和纯燃料(如正己烷,正辛烷,正十二烷和正十六烷)组成的水乳化液体。由透明管道制成的燃烧室安装有火花电极,细小的石英纤维以悬浮燃料滴,并设有百叶窗以使燃烧的气体在顶端逸出。提供了高速摄影机,以摄影观察由传播的火焰点燃的每个液滴。纯燃料液滴的点火延迟随初始液滴直径的增加和燃料挥发性的降低而单调增加。初始液滴直径对点火延迟的影响随着燃料挥发性的增加而降低。随着高挥发性燃料的体积浓度的增加,二元燃料小滴的点火延迟减小。二元燃料的点火延迟根据初始液滴直径显示出最小值和最大值。随着更高挥发性燃料浓度的增加,最小和最大点火延迟直径减小。另一方面,对于乳化燃料,点火延迟随着初始液滴直径的增加和水含量的增加而增加。当液滴通过高挥发性燃料的液滴时,液滴后面的传播火焰的一部分向未充气气体凸出,而对于低挥发性燃料则火焰保持平坦。液滴后面的传播火焰的变形长度随着高挥发性燃料浓度的增加而增加。

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