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COMBUSTION OF A GAS-TO-LIQUID-BASED ALTERNATIVE JET FUEL: EXPERIMENTAL AND DETAILED KINETIC MODELING

机译:基于气体到液体的替代性喷气燃料的燃烧:实验和详细的运动学建模

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摘要

The kinetics of oxidation of blends of gas-to-liquid (GtL) jet fuel with 20% vol. of 1-hexanol was studied. New experimental results were obtained using a jet-stirred reactor (p = 10 bar, constant mean residence time of I s, over the temperature range 550-1150 K, and for equivalence ratios of 0.5,1, and 2). Concentration profiles of readouts, stable intermediates, and final products were obtained by probe sampling followed by on-line and off-line gas chro-matography analyses and on-line Fourier transformed infra-red spectrometry. A comparison with corresponding results for Jet A-1 and pure GtL showed these fuels have similar combustion properties. The oxidation of the GtL-hexanol fuel under these conditions was modeled using a detailed.kinetic reaction mechanism consisting of 8217 reactions and 2185 species and a 4-component surrogate fuel mixture (n-decane, iso-octane, n-propyl cyclohexane, and 1-hexanol). The proposed kinetic model showed good agreement with the presently reported jet-stirred reactor concentration profiles.
机译:体积比为20%的气液(GtL)喷气燃料混合物的氧化动力学。研究了1-己醇的含量。使用射流搅拌反应器获得了新的实验结果(p = 10 bar,在5500-1150 K的温度范围内,当量比为0.5、1和2时,恒定的平均停留时间为s)。通过探针采样,在线和离线气相色谱分析以及在线傅立叶变换红外光谱法获得读数,稳定的中间体和最终产物的浓度曲线。与Jet A-1和纯GtL的相应结果进行的比较表明,这些燃料具有相似的燃烧特性。使用详细的动力学反应机理对GtL-己醇燃料在这些条件下的氧化过程进行建模,该机理由8217个反应和2185种物质和4组分替代燃料混合物(正癸烷,异辛烷,正丙基环己烷和1-己醇)。所提出的动力学模型与目前报道的喷射搅拌反应器浓度曲线显示出良好的一致性。

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