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Reacting Pressurized Spray Combustor Dynamics, Part 1. Fuel Sensitivities and Blowoff Characterization

机译:加压喷雾燃烧器动力学的反应,第1部分。燃料敏感性和排污特性

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Blowoff sets important operational limits on a combustor system. While blowoff is intrinsically a system-dependent phenomenon, it is also dependent on the chemical and physical properties of the fuel. This paper describes an experimental study of the lean blowout limits of eight liquid fuels in a swirl-stabilized combustor, with data for both a pressure atomizer and an airblast atomizer. Three of the fuels were traditional jet fuels (an average Jet-A, JP-5, and JP-8) and the remaining five fuels spanned a range of physical and kinetic properties. These experiments were performed at a combustor pressure of 345 kPa and an air temperature of 450 K. In addition to some sensitivity of blowoff conditions to the thermal state of the combustor, results also clearly show sensitivities to fuel composition. Strong correlations were observed for pressure atomizer blowoff with fuel physical properties, particularly for boiling point temperature, indicating that fuels less easily atomized and vaporized are harder to blow off. These results are consistent with the idea that delaying atomization and/vaporization, and therefore reducing the level of premixing that drives the local fuel-air ratio towards the very lean global fuel/air ratio, is advantageous in order to promote regions of locally elevated flame temperatures. We suggest that this behavior occurs when the air preheat temperature is above the fuel flashpoint, as a similarly good correlation with boiling point temperature but with the opposite trend, has been previously reported in a study obtained for preheat temperatures below the fuel flashpoint. In contrast, the airblast results do not show strong correlations with fuel physical properties. Rather, the best correlation of the airblast atomizer results is with the percentage of iso-paraffms in the fuel. We speculate that this reflects a sensitivity to kinetic properties of the fuel, as the superior atomization characteristics of the airblast atomizer may de-emphasize the importance of physical properties.
机译:吹乱在燃烧器系统上设定了重要的操作限制。虽然吹出是内在的系统依赖现象,但它也取决于燃料的化学和物理性质。本文介绍了涡旋稳定燃烧器中八个液体燃料的贫井喷限制的实验研究,具有压力雾化器和空燃雾化器的数据。其中三个燃料是传统喷射燃料(平均喷射-A,JP-5和JP-8),剩余的五种燃料跨越一系列物理和动力学性质。这些实验在345kPa的燃烧室压力和450k的空气温度下进行。除了向燃烧器的热状态的吹气条件的一些灵敏度之外,结果也明确显示燃料组合物的敏感性。观察到具有燃料物理性质的压力雾化器吹气的强相关性,特别是对于沸点温度,表明燃料较容易雾化和蒸发更难吹掉。这些结果与延迟雾化和/蒸发的想法一致,因此降低了驱动局部燃料空气比朝向非常精益的全球燃料/空气比的预混合水平,是有利的,以促进局部升高的火焰区域温度。我们建议当空气预热温度高于燃料闪光点时,通常发生这种行为,作为与沸点温度的同样良好的相关性,但具有相反的趋势,先前已在用于预热温度下方的燃料闪光点以下的研究中。相比之下,空发挥结果并不与燃料物理性质显示出强烈的相关性。相反,空转雾化器结果的最佳相关性具有燃料中的iso-maraffms的百分比。我们推测这反映了对燃料的动力学性质的敏感性,因为空气雾化器的优异雾化特性可以解除物理性质的重要性。

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