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Studies on the mixing of liquid jets and pre-atomized sprays in confined swirling air flows for lean direct injection combustion.

机译:研究液体射流和预雾化喷雾在有限的旋流中的混合,以实现稀薄的直接喷射燃烧。

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A lean direct injection (LDI) combustion concept was introduced recently to obtain both low NO{dollar}sb{lcub}rm x{rcub}{dollar} emissions and high performance for advanced aircraft gas turbine engines. It was reported that pollutant emissions, especially NO{dollar}sb{lcub}rm x{rcub},{dollar} in a lean combustion mode depend significantly on the degree of mixing (mixedness) of supplied air and liquid fuel droplets. From a viewpoint of environmental protection, therefore, uniform mixing of fuel and air in a very short period of time, i.e., well-stirred mixing, is crucially important in the LDI combustion mode.; In the present study, as the first stage toward understanding the combustion phenomena in a lean direct injection (LDI) mode, the hydrodynamic behavior of liquid jets and pre-atomized sprays in confined swirling air flows is investigated. Laser-based flow visualization and image analysis techniques are applied to analyze the instantaneous motion of the mixing process of the jets and pre-atomized sprays. Statistical analysis system (SAS) software is utilized to analyze the experimental data, and correlate experimental parameters. Statistical parameters, such as centrality, degree of spread, and total area ratio of particles, are defined in this study, and used to quantify the mixedness (degree of mixing) of liquid particles in confined geometry.; Two empirical equations are obtained to predict jet intact lengths and spray angles, respectively, in confined swirling air flows. It is found that initial jet characteristics, such as intact length and spray angle, determine the mixing of the liquid particles resulting from the jet. It is verified that image analysis is feasible in quantitative determination of the mixedness of liquid particles. Even though substantial improvements in liquid fuel injector systems are required before they can be considered adequate for LDI combustion at high pressure and high temperature, the results and ideas obtained from the present study will help engineers find better mixing methods for LDI combustors.
机译:最近引入了稀薄的直接喷射(LDI)燃烧概念,以获取低NOx排放和先进飞机燃气涡轮发动机的高性能。据报道,在稀薄燃烧模式下的污染物排放,尤其是NO x,很大程度上取决于所供应的空气和液体燃料液滴的混合程度(混合度)。因此,从环境保护的观点来看,在LDI燃烧模式中,在很短的时间内均匀混合燃料和空气,即充分搅拌是至关重要的。在本研究中,作为了解稀薄直接喷射(LDI)模式下燃烧现象的第一步,研究了受限旋流中液体射流和预雾化喷雾的流体动力学行为。基于激光的流动可视化和图像分析技术被应用于分析射流和预雾化喷雾混合过程的瞬时运动。统计分析系统(SAS)软件用于分析实验数据,并关联实验参数。这项研究定义了统计参数,例如中心度,扩散程度和颗粒的总面积比,并用于量化受限几何形状中液体颗粒的混合度(混合度)。获得两个经验方程,分别预测有限的涡旋气流中的射流完整长度和喷射角度。发现初始喷射特性,例如完整长度和喷射角度,决定了由喷射产生的液体颗粒的混合。证实了图像分析在定量确定液体颗粒的混合性方面是可行的。即使需要对液体燃料喷射器系统进行重大改进,才可以认为它们足以在高压和高温下进行LDI燃烧,但从本研究中获得的结果和构想将有助于工程师为LDI燃烧器找到更好的混合方法。

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