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SULFUR DEPOSIT FORMATION IN JET FUEL AT HIGH THERMAL STRESSING TEMPERATURES

机译:在高热应力温度下的喷射燃料中硫沉积物形成

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Aviation fuel thermal stability is defined by its resistance to deposit formation while undergoing thermal stress. Thermal deposits have normally been characterized visually or when quantified, as a total deposit mass or specifically related to carbon mass. It has been observed that some fuels, specifically MEROX treated, tend to form high levels of sulfur containing deposits, some times of greater mass of total sulfur than carbon. This work describes sulfur deposit formation quantified by total sulfur analysis using a LECO CS-244 from jet fuels over a range of temperatures (300 - 400°C) and flow conditions (0.5 - 2 ml/minute) in a single pass thermal stability rig. It was observed that sulfur deposit mass increased with temperature and decreased with increasing flow rate. Sulfur deposition rate also decreased with total mass of fuel stressed suggesting influences from changes in deposit thermal conductivity on the reaction vessel surface.
机译:航空燃料热稳定性由其在经历热应力的同时对沉积物形成的抵抗来限定。 热沉积通常已经在视觉上或定量时表征,作为总沉积物或与碳质量有特异性。 已经观察到,一些燃料,特别是Merox处理,倾向于形成高水平的含硫沉积物,总硫的一定时间比碳大致含量。 该作品描述了通过在单通热稳定钻机的一系列温度(300-400℃)和流动条件(0.5-2ml /分钟)范围内的喷射燃料的LeCo CS-244通过总硫分析量化的硫沉积物形成。 。 观察到硫沉积物质量随温度的增加并随着流速的增加而降低。 硫沉积速率也随着燃料总质量的燃料胁迫,表明从反应容器表面上的沉积物导热率的变化影响。

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