首页> 外文期刊>Applied Catalysis, A. General: An International Journal Devoted to Catalytic Science and Its Applications >Partial oxidation of methane to syngas at high space velocities over Rh-coated spheres
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Partial oxidation of methane to syngas at high space velocities over Rh-coated spheres

机译:Rh包覆球体上高空速下甲烷部分氧化为合成气

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摘要

The effect of space velocity on the partial oxidation of methane using different support geometries has been studied. While on a foam alumina monolith syngas selectivity drops as space velocity is increased above 4 x 105 h~(-1), the use of non-porous alumina spheres as the support allows high reactant conversions and syngas selectivities even at space velocities of 1.8 x 106h~(-1). The differences between monoliths and spheres are discussed in order to understand why spheres give superior results. It is suggested that differences in heat transfer within the two support geometries may playa major role in the different results between spheres and monoliths. A convective heat transfer model suggests that higher rates of convection in a monolith will lead to lower front temperatures than in a sphere bed, a trend that becomes important at high space velocities in leading to blowout and lower syngas selectivities.
机译:研究了不同载体几何结构下空速对甲烷部分氧化的影响。在泡沫氧化铝上,整料的合成气选择性随空速增加到4 x 105 h〜(-1)以上而下降,但使用无孔氧化铝球作为载体仍可实现高反应物转化率和合成气选择性,即使空速为1.8 x 106h〜(-1)。讨论了整体结构和球体之间的差异,以了解为什么球体会产生更好的结果。建议在两个支撑几何结构内传热的差异可能在球体和整料之间的不同结果中起主要作用。对流传热模型表明,整体结构中较高的对流速率将导致比球形床更低的前部温度,这种趋势在高空速下变得重要,从而导致井喷和较低的合成气选择性。

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