摘要
为了评价煤基费托合成航空替代燃料的雾化和点火性能,利用单头部矩形燃烧室对国产煤基费托燃料、传统航空煤油RP-3以及二者50:50混合燃料的雾化索太尔平均直径SMD和贫油点火边界进行了实验研究。实验结果显示,常温条件下,三种燃料的雾化SMD和贫油点火边界都有相同的变化趋势,SMD的减小趋势在供油压力达到0.5MPa后变缓,贫油点火边界的扩展趋势在燃烧室压降达到2.0%后变缓;相比航空煤油RP-3,煤基费托燃料的雾化性能和点火性能稍差,通过相互掺混可以得到改善。使用响应面模型(RSM)研究总结了雾化SMD的经验关系式,分析了燃料雾化和蒸发过程对其点火性能的影响。
In order to investigate the atomization and ignition performance of coal-based Fischer-Tropsch synthetic aviation alternative fuels, a single-module rectangular combustor was used to experiment the atomiza- tion Sauter mean diameter (SMD) and lean ignition limit of the domestic coal-based F-T synthesis, traditional aviation kerosene RP-3 and 50:50 mixture of both fuels. Experiment results show that, the atomization and lean ignition limit of the three fuels share the same trends under normal temperature respectively, where the decreas- ing trend of SMD slows after fuel injection pressure reaches 0.5MPa and the expansion trend of lean ignition limit slows after combustor pressure drop reaches 2.0%. Atomization and ignition performance of the F-T fuel are poor- er than that of aviation kerosene RP-3, which can be improved by mixing with each other. The atomization SMD empirical relationship was summarized by using the response surface methodology (RSM), and the effects of at- omization and evaporation process on ignition performance were analyzed.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2017年第11期2622-2627,共6页
Journal of Propulsion Technology
基金
国家自然科学基金(51306010)
北京市自然科学基金(3152020)
关键词
费托合成
替代燃料
雾化
响应面模型
贫油点火
Fischer-Tropsch synthesis
Alternative fuel
Atomization
Response surface methodology
Lean ignition