PUFFING AND MICROEXPLOSION IN SECONDARY DROPLETS

P. Strizhak, D. Antonov
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Abstract

Secondary atomization of droplets (in the partial or full fragmentation regime) in multiphase and multicomponent fuel §ows is a promising technology that can minimize fuel consumption, improve the combustion dynamics, reduce anthropogenic emissions, stabilize fuel injection in a combustion chamber, and reduce the equipment wear [1, 2]. The most promising secondary atomization schemes involve droplet droplet collisions in intersecting fuel jets [3], droplet collisions with a solid surface in the form of walls, rings, meshes, and ledges [4], microexplosion, and pu©ng [5]. As a result of a microexplosion, the droplets of multiphase and multicomponent fuels break up to form an array of liquid fragments with a size of 1 100 μm [5]. The aim of this work is experimental research of pu©ng and microexplosion in secondary droplets. The number and radii of secondary fragments (child droplets) were analyzed by Shadow Photography (SP). Three approaches have been used to improve the accuracy of the experimental ¦ndings and to estimate their repeatability in a series of experiments. The measurements did not deviate by more than 5%. From the experiments conducted, the present authors managed to ¦nd the cause of signi¦- cant di¨erences in the characteristics of child droplets being formed in the course of microexplosion and pu©ng of two-liquid droplets for di¨erent formation regimes and identical heating conditions. After the research ¦ndings have been generalized, it became possible to determine the ranges of variation for the main parameters at which the maximum amount of child droplets with the required component composition could be obtained. In particular, the authorshave singled out the maps with multiple input parameters that can be used in the technologies of secondary fragmentation for the intensi¦cation of fuel mixing and combustion, puri¦cation of liquids, intensi¦cation of phase transitions, and heat exchange in power generation units.
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二次液滴的膨化和微爆炸
在多相和多组分燃料燃烧室中,液滴的二次雾化(在部分或完全破碎状态下)是一项很有前途的技术,可以最大限度地减少燃料消耗,改善燃烧动力学,减少人为排放,稳定燃烧室的燃油喷射,减少设备磨损[1,2]。最有前途的二次雾化方案包括在相交的燃料射流中液滴碰撞[3],液滴与固体表面以壁、环、网格和壁架的形式碰撞[4],微爆炸和pu©ng[5]。在微爆炸过程中,多相、多组分燃料的液滴破碎,形成尺寸为1100 μm的液体碎片阵列[5]。本论文的目的是对二次液滴的微爆炸和喷射进行实验研究。采用阴影摄影法(SP)分析了次生碎片(子液滴)的数量和半径。本文采用了三种方法来提高实验结果的准确性,并在一系列实验中估计其可重复性。测量结果的偏差不超过5%。通过实验,找出了在不同的形成条件和相同的加热条件下,微爆炸过程中形成的子液滴和形成的双液液滴的特性存在显著差异的原因。在对研究结果进行推广之后,就有可能确定主要参数的变化范围,在此范围内,可以获得具有所需成分组成的最大数量的子液滴。特别是,作者挑选了可用于二次破碎技术的多输入参数图,以加强燃料混合和燃烧、液体净化、相变强化和发电机组的热交换。
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О МЕХАНИЗМЕ АЭРОАКУСТИЧЕСКОЕО ИНИЦИИРОВАНИЯ ПУЛВСИРУЮЩЕЕО КВАЗИДЕТОНАЦИОННОЕО ЕОРЕНИЯ В ЭЖЕКТОРНОМ ПУЛВСИРУЮЩЕМ ВОЗДУШНО-РЕАКТИВНОМ ДВИЕАТЕЛЕ НОВЫЕ РЕЗУЛЬТАТЫ ИССЛЕДОВАНИЙ РАСПРОСТРАНЕНИЯ ДЕТОНАЦИИ В ВЯЗКОМ ТУРБУЛЕНТНОМ ТЕЧЕНИИ В КАНАЛЕ IMPROVEMENT OF IGNITION SYSTEM OF DETONATION ENGINES WITH AN INITIATED MICROWAVE SUBCRITICAL STREAMER DISCHARGE О НЕКОТОРЫХ ДИНАМИЧЕСКИХ ЯВЛЕНИЯХ ПРИ РАСПРОСТРАНЕНИИ ГАЗОВОЙ ДЕТОНАЦИИ В СРЕДЕ С ПЕРИОДИЧЕСКОЙ НЕОДНОРОДНОСТЬЮ ОПРЕДЕЛЕНИЕ ВРЕМЕН ИНДУКЦИИ И РЕАКЦИИ СМЕСЕЙ ВОДОРОДА С ВОЗДУХОМ ПРИ ВЫСОКИХ ТЕМПЕРАТУРАХ
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