高温高压环境下RP-3航空煤油单液滴的加热与蒸发特性研究OA
Investigation on Heating and Vaporization Characteristics of Single RP-3 Aviation Kerosene Droplet at Elevated Temperature and Pressure
RP-3航空煤油是当前国内最常用的商用喷气燃料,煤油液滴在航空发动机燃烧室中的蒸发直接影响燃料的雾化效果、空燃混合气的形成和燃烧质量.本文以单个RP-3航空煤油液滴为研究对象,选取正十二烷、2,5-二甲基己烷、甲苯作为替代燃料,提出了一个考虑自然对流效应的高温高压环境下多组分液滴蒸发模型.利用自主搭建的试验装置得到了环境压力为1MPa、环境温度为473~673K下RP-3煤油单液滴在蒸发过程中的液滴直径变化.模型预测结果与试验结果的对比验证了模型的准确性.通过模型预测了不同环境参数下三组分替代物液滴直径、内部温度分布、各组分质量分数分布和液滴寿命等参数的瞬态变化,定量分析了不同高温条件下环境压力对单液滴蒸发特性的影响.结果表明,液相内部的传热传质会影响多组分液滴的蒸发速率,且液相扩散阻力造成了液相内部组分质量分数与温度空间分布的不均匀性.环境压力对RP-3煤油液滴蒸发寿命的影响随环境温度的变化而变化.当环境温度低于正十二烷的临界温度(658.25K)时,液滴寿命与环境压力的关系不是单调的,液滴寿命随环境压力的增加先增后减;而当环境温度超过658.25K时,液滴寿命随环境压力的升高而单调减小.这是因为在高温高压环境中,环境压力的升高能显著增大自然对流传热传质强度,而自然对流超过一定强度时,能明显促进液滴蒸发.上述研究有利于认识液滴内部组分扩散过程,从源头上为未来高性能低污染发动机的优化设计提供依据与参考.
RP-3 aviation kerosene is a commercial jet fuel commonly employed in China.The evaporation of aviation kerosene droplets in the aeroengine combustion chamber directly affects the fuel atomization performance,the formation of air-fuel mixture,and combustion quality.To accurately predict the heating and vaporization characteristics of single RP-3 kerosene droplet,the blend of n-dodecane,2,5-dimethylhexane and toluene was selected as the surrogate fuel.And a multi-component droplet evaporation model considering the natural convection effect at elevated temperature and pressure was proposed in the present study.Based on the self-developed experimental apparatus,the temporal variations of the RP-3 kerosene droplet diameter were obtained for an ambient pressure of 1MPa at ambient temperatures of 473K to 673K.The accuracy of the model was validated by the comparison between the simulation results and experimental results.The predictions of the parameters including diameter,internal temperature distribution,component mass fraction distribution and lifetime of three-component surrogate fuel by the new-proposed model were used to quantitatively analyze the effect of ambient pressure on the evaporation characteristics of individual droplet under various ambient temperatures.The results indicated that the heat and mass transfer inside the liquid phase can affect the evaporation rate of multi-component droplets,and the liquid diffusion resistance leads to the heterogeneity of the distribution of internal temperature and component mass fraction inside the liquid phase.The impact of environmental pressure on the RP-3 kerosene droplet lifetime strongly depends on environmental temperature.When the ambient temperature is below the critical temperature of n-dodecane(658.25K),the relationship between droplet lifetime and ambient pressure is not monotonic,but first increases and then decreases with the increase of ambient pressure.When the ambient temperature exceeds 658.25K,the droplet lifetime monotonically decreases as ambient pressure increases.This can be attributed to the fact that in high temperature and pressure environment,the increase of ambient pressure can significantly increase the heat and mass transfer intensity of natural convection.When natural convection exceeds a certain intensity,it can obviously promote droplet evaporation.The study above is conducive to underseand the diffusion process of the internal for the optimized design of future high-performance low-pollution engines from the source.
印晶;梁勇;张龙飞;薛书勤;刘兵;周致富
西安交通大学 动力工程多相流国家重点实验室,陕西 西安 710049西安航天动力测控技术研究所,陕西 西安 710025
单液滴蒸发航空发动机自然对流RP-3航空煤油三组分替代
single droplet evaporationaero-enginenatural convectionRP-3 aviation kerosenethree-component representative
《航空科学技术》 2024 (003)
55-69 / 15
国家自然科学基金(52176163);航空科学基金(2019ZB070002) National Natural Science Foundation of China(52176163);Aeronautical Science Foundation of China(2019ZB070002)
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