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Investigation of Short Contact Time Reactors for Regeneratively Cooled Hypersonic Vehicles

机译:蓄冷超音速飞行器短接触时间反应堆的研究

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For hydrocarbon-based fuels to be viable as scramjet fuels they must be able to absorb heat from engine structures in the form of sensible, latent, and chemical enthalpies, while attempting to minimize coke formation. In this study, a short contact time catalytic reactor was used to achieve these ends. Experiments were performed using a series of different catalysts (Pt - A1_2O_3, Rh - A1_2O_3, and zeolite) on a set of logistical fuels (JP-7, JP-8, JP-10, and S-8, a synthetic hydrocarbon fuel currently being investigated by the U.S. Air Force). Experiments were performed at low (1-3 atmospheres) and elevated (40-50 atmospheres) pressures, at temperatures of 650 and 750℃. The production of gas- and liquid-phase species was measured as a function of pressure, temperature, residence time, and catalyst formulation. Results show the production of small (H_2, C_1-C_3) species in the gas phase, with a shift from hydrogen and ethylene formation at low pressures toward methane and ethane formation at elevated pressures. In addition, significant coke formation at elevated pressures for all of the fuels was witnessed. Detailed kinetic modeling identified shortcomings in models used for describing the pyrolysis of these fuels.
机译:为了使碳氢化合物燃料能作为超燃喷射燃料可行,它们必须能够以合理的,潜在的和化学的焓形式从发动机结构吸收热量,同时试图将焦炭的形成降至最低。在这项研究中,短接触时间催化反应器用于实现这些目的。使用一系列不同的催化剂(Pt-A1_2O_3,Rh-A1_2O_3和沸石)对一组后勤燃料(JP-7,JP-8,JP-10和S-8,目前为合成烃燃料)进行了实验正在被美国空军调查)。在低压(1-3个大气压)和高压(40-50个大气压)下,在650和750℃的温度下进行实验。测量气相和液相物质的产生与压力,温度,停留时间和催化剂配方的关系。结果表明,在气相中产生小的(H_2,C_1-C_3)物种,从低压下的氢气和乙烯形成转变为高压下的甲烷和乙烷形成。另外,在高压下所有燃料均会形成大量焦炭。详细的动力学建模发现了用于描述这些燃料热解的模型中的缺陷。

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