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Kinetic Modeling of Thermal and Catalytic Cracking of Paraffinic Surrogate Fuels Relevant to Hypersonic Applications

机译:与超音速应用相关的石蜡代用燃料的热催化裂化动力学模型

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Endothermic heat sink capacity of fuels is important for the thermal management of hypersonic vehicles. Chemical kinetic models of multi-component hydrocarbon fuels can be used to estimate the endothermic heat sink capacity, but require knowledge of the chemical kinetic behavior of these complex fuels during cracking. The heat sink capacity of these fuels is largely controlled by the ratio of olefins to n-paraffins produced during the thermal/catalytic cracking. Therefore, it is important to validate the model for product selectivity for accurate prediction of endothermic heat sink capacity. A detailed chemical kinetic model for the thermal and catalytic cracking of n-paraffins was developed and validated over a range of experimental conditions including hypersonic relevant conditions. The model includes a detailed gas-phase pyrolysis kinetic model for C_1 to C_(16) n-paraffins along with a surface kinetic model for n-octane on H-ZSM-5 zeolite catalyst. It was demonstrated that gas-phase kinetic model coupled with the surface kinetic model was able to predict the endothermic heat sink capacity correctly during the thermal and catalytic cracking of «-octane. The model also predicts the product selectivity of thermal and catalytic cracking reasonably well.
机译:燃料的吸热散热能力对于高超声速车辆的热管理非常重要。可以使用多组分烃类燃料的化学动力学模型来估计吸热散热器的吸热能力,但需要了解这些复杂燃料在裂化过程中的化学动力学行为。这些燃料的散热能力在很大程度上由在热/催化裂化过程中产生的烯烃与正链烷烃的比例来控制。因此,重要的是验证产品选择性模型,以准确预测吸热散热器的容量。已开发了正构烷烃热裂解和催化裂解的详细化学动力学模型,并在包括高超声速相关条件在内的一系列实验条件下进行了验证。该模型包括C_1至C_(16)正链烷烃的详细气相热解动力学模型,以及H-ZSM-5沸石催化剂上正辛烷的表面动力学模型。结果表明,气相动力学模型与表面动力学模型相结合,能够正确地预测正辛烷的热裂化和催化裂化过程中的吸热散热能力。该模型还可以很好地预测热裂解和催化裂解的产品选择性。

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