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Combustion temperature, Pressure and Products at Chemical Equilibrium of H-Air, NH-Air and C H-Air Fuel Mixtures

机译:H-AIR,NH-AIR和C H空气燃料混合物化学平衡下的燃烧温度,压力和产品

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For a thermodynamic analysis of engines and gas turbines cycles working with hydrogen, ammonia and propane as fuels, the thermodynamic properties of the combustion gaseous must be available in the form of equations or charts. This paper deals with the development of a thermodynamic model for the equilibrium products composition with superimposed kinetic NO and CO rates of formation. This has been used to compare the predicted species concentration, dissociation and NO and CO rates of formation concentration, dissociation and NO and CO rates of formation levels from different gases fuel-air mixtures combustion. The results of computations of the combustion products and kinetic NO and CO rates of formation at specified equilibrium temperatures, pressurs, and equivalence ratios are plotted in graphs and given in tables. For calculations of the combustion products at chemical equilibrium a set of 6 equilibrium equations is enlarged by the energy and mass balance equations is applied. Kinetic mechanisms for NO and CO rate of formation assuming other species at equilibrium and steady state for N atoms are also included. The results are obtained for the following conditions:---(1) H-Air, NH-Air and C H -Air gases fuel Mixtures. (2) Range of pressurees, p = 1-100 ata. (3) Range of temperatures, T = 2000-5000 K. (4) Range of equivalence ratos PHI = 0.6-2.0 Results of a few selected conditions are plotted.
机译:对于用氢气,氨和丙烷与燃料一起使用的发动机和燃气轮机循环的热力学分析,燃烧气体的热力学性能必须以方程或图表的形式获得。本文涉及具有叠加动力学NO和形成的均衡动力学产品的热力学模型。这已被用于比较从不同气体燃料 - 空气混合物燃烧中的预测物种浓度,切离和NO,形成浓度,离解和NO和CO率的形成水平的CO率。在规定的平衡温度,压力和等效比下绘制燃烧产物和动力学NO和CO率的计算结果在图表中绘制,并在表格中给出。对于化学平衡的燃烧产物的计算,通过施加能量和质量平衡方程,通过施加一组6平衡方程。还包括否则不包括在N原子的平衡和稳态处的其他物种的NO和CO速率的动力学机制。结果是在以下条件下获得的:---(1)H-空气,NH-AIR和C H-航空气体燃料混合物。 (2)压力范围,P = 1-100 ATA。 (3)温度范围,T = 2000-5000 K.(4)等当量RATOS PHI = 0.6-2.0的结果绘制了一些选定条件的结果。

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