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Combustion simulations of the fuels for advanced combustion engines in a homogeneous charge compression ignition engine

机译:均质充量压缩点火发动机中用于高级内燃机的燃料的燃烧模拟

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Numerical simulations of combustion have been performed for a homogeneous charge compression ignition engine operating on multi-component reference diesel fuels. Two surrogate representation methods were used to describe the nine fuels for advanced combustion engines. The first method of surrogates, denoted as physical-surrogate components, was formulated to describe the fuel's physical properties by matching its distillation profile, specific gravity, lower heating value, hydrogen-to-carbon ratio, and cetane index with measured data. The second method of surrogates, denoted as chemical-surrogate components, was introduced to represent the chemistry of the fuel components using a new group chemistry representation model. In the model, the fuel components in the physical-surrogate components and chemical-surrogate components are related through the classification of chemical structures of the components, i.e. the component in the physical-surrogate components are grouped based on their chemical classes and the chemistry of each group is calculated using a chemical kinetics mechanism (MultiChem) that represents the combustion characteristics of its chemical class. This MultiChem mechanism includes reduced reaction mechanisms for the four main surrogate hydrocarbon chemistry components of diesel fuel, n-paraffins, iso-paraffins, naphthenes, and aromatics, with two n-paraffins to provide the ability to mimic molecular weight effects. The computations were performed using a multi-dimensional computational fluid dynamic code, KIVA-ERC-CHEMKIN, and the results show that the predictions of the present multi-component combustion models are in good agreement with experimental measurements. The combustion characteristics of the fuels for advanced combustion engines are well represented and the present models are well suited for practical engine computations.
机译:对于使用多组分参考柴油燃料运行的均质充量压缩点火发动机,已经进行了燃烧的数值模拟。使用两种替代表示方法来描述高级内燃机的九种燃料。通过将代用燃料的蒸馏曲线,比重,较低的热值,氢碳比和十六烷指数与实测数据相匹配,制定了第一种代用燃料的方法,称为物理代用组分,以描述燃料的物理性质。引入了第二种替代方法,称为化学替代组分,使用新的组化学表示模型来代表燃料组分的化学。在该模型中,物理替代组分中的燃料组分和化学替代组分通过组分的化学结构分类而相互关联,即物理替代组分中的组分根据其化学类别和化学成分进行分组。每组均使用代表其化学类别的燃烧特性的化学动力学机制(MultiChem)进行计算。这种MultiChem机制包括针对柴油,正链烷烃,异链烷烃,环烷烃和芳烃的四个主要替代碳氢化合物化学成分的简化反应机理,其中两个正链烷烃具有模拟分子量效应的能力。使用多维计算流体动力学代码KIVA-ERC-CHEMKIN进行了计算,结果表明,当前的多组分燃烧模型的预测与实验测量值非常吻合。很好地表示了用于高级内燃机的燃料的燃烧特性,并且本模型非常适合于实际的发动机计算。

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