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Thermal oxidation coking of aviation kerosene RP-3 at supercritical pressure in helical tubes

机译:螺旋管中超临界压力下航空煤油RP-3的热氧化焦化

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The mechanism of thermal oxidation coking of aviation kerosene RP-3 at a supercritical pressure of 5 MPa in helical tubes was analyzed. The bulk temperature of the fuel was varied from 400 K to 723 K, and the mass flux was varied from 393 kg/m(2) s to 1178 kg/m(2) s. Four types of helical tubes with different helical diameters were bent and tested for a maximum duration of 5 h. The total coking amount and distribution were analyzed using weighing method, and the standard error was less than 0.07 mg. The results indicate that coking distribution is more uniform than in the case of a straight tube, and that there is no prominent coking peak because of the effect of centrifugal force. The maximum total coking amount among all the experiments decreased by approximately 69.5% compared with that in a straight tube. Through measurements performed using a scanning electron microscope, three main types of coking morphologies were observed: thin coking layer, dense clumps, and crystalline particles. Moreover, various types of coking elements were detected under different working conditions. (C) 2017 Elsevier Ltd. All rights reserved.
机译:分析了在螺旋管中的5MPa的超临界压力下的航空酮烯RP-3的热氧化焦化机理。燃料的体积温度从400k到723k变化,质量磁通量从393kg / m(2)s变化至1178kg / m(2)s。具有不同螺旋直径的四种类型的螺旋管弯曲并测试最大持续时间为5小时。使用称重方法分析总焦化量和分布,标准误差小于0.07毫克。结果表明,焦化分布比在直管的情况下更均匀,并且由于离心力的影响,没有突出的焦化峰。与直管中的所有实验中,所有实验中的最大总焦化量减少了大约69.5%。通过使用扫描电子显微镜进行的测量,观察到三种主要类型的焦化形态:薄的焦化层,密集块和结晶颗粒。此外,在不同的工作条件下检测各种类型的焦化元素。 (c)2017 Elsevier Ltd.保留所有权利。

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