A new surrogate fuel of RP3 kerosene
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摘要: 为了遴选出符合RP-3航空煤油物理与化学特性的模拟替代燃料,综合分析了RP-3航空煤油的物理与化学特性。针对其物理与化学特性,确定了RP-3航空煤油模拟替代燃料的遴选指标(包括摩尔质量、氢碳比、十六烷值与低热值)。针对遴选指标,提出了由正癸烷、正十二烷、异十六烷、甲基环己烷及甲苯等五种组分组成的RP3航空煤油模拟替代燃料,并对该模拟替代燃料中各组分的摩尔分数进行了优化。同时,对比分析了不同温度下该模拟替代燃料与RP3航空煤油的密度与运动黏度。结果表明,当该模拟替代燃料中正癸烷、正十二烷、异十六烷、甲基环己烷及甲苯的摩尔分数分别为14%、10%、30%、36%与10%时,该模拟替代燃料的摩尔质量、氢碳比、十六烷值与低热值与RP3航空煤油的相应数据非常吻合。同时,不同温度下该模拟替代燃料的密度与运动黏度变化趋势与RP-3航空煤油吻合较好。Abstract: In order to select the surrogate fuel with the same physical and chemical properties as RP-3 kerosene, the physical and chemical properties of RP3 kerosene were analyzed. According to the physical and chemical properties of RP3 kerosene, the selection criterions of the RP3 kerosene surrogate fuel (including the molecular mass, hydrogencarbon ratio, cetane number and lower heating value) were determined. Based on the selection criterions, a fivecomponent RP-3 kerosene surrogate fuel comprising ndecane, n-dodecane, iso-cetane, methylcyclohexane and toluene was presented, and the mole fractions of these five components were optimized. Furthermore, the densities and kinematic viscosities of the surrogate fuel and RP3 kerosene were contrastively analyzed at different temperatures. The results show that the molecular mass, hydrogencarbon ratio, cetane number and lower heating value of the surrogate fuel, which comprise 14% ndecane/10% ndodecane/30% isocetane/36% methylcyclohexane/10% toluene (mole fraction), agree well with the corresponding criterions of RP3 kerosene. At the same time, the variation trends of the densities and kinematic viscosities of the surrogate fuel agree well with the corresponding experimental data of RP3 kerosene at different temperatures.
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Key words:
- RP-3 kerosene /
- surrogate fuel /
- selection criterion /
- density /
- kinematic viscosity
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