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煤油催化重整可燃燃气发生器的试验研究 被引量:2

Experimental Researches on Flammable Gas Generator of Kerosene with Catalytic Reforming Reaction
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摘要 设计了新型煤油催化重整燃气发生器,在较大油量和较高压力情况下,进行了一系列相关参数的影响试验.试验结果表明:在催化温度较高、头部余气系数保持在0.6~0.8时,其出口燃气温度为400~700℃,可燃气体成分占15%~30%,氢气体积分数最高可达16%,从而可为超燃冲压发动机提供良好的高温含氢可燃燃气,有利于超燃室内的点火和稳定燃烧. A new type of kerosene gas generator for catalytic reforming reaction was designed. Under high fuel flow rate and high pressure, the effects of different parameters on catalytic reaction were studied through a series of experiments. The resalts show that the exit flammable gas temperature of 400-700 ℃ and the gas composition of 15%-30% will be obtained when the excessive air coefficient is controlled between 0. 6-0. 8 and the catalytic temperature reaches about 500-700 ℃. The hydrogen quantum of 16% will be achieved in the high temperature fuel-rich flammable gases, which can be introduced into the scramjet and will be helpful to its ignition and stable combustion process.
出处 《燃烧科学与技术》 EI CAS CSCD 北大核心 2009年第2期97-102,共6页 Journal of Combustion Science and Technology
关键词 催化重整 煤油 燃气发生器 catalytic reforming kerosene gas generator
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参考文献7

  • 1Waltrup P J.Liquid-Fueled Supersonic Combustion Ramjets:A Research Perspective of the Past,Present and Future[R].Reno,USA:AIAA 86-0158,1986.
  • 2崔可润,高孝洪,ТнмошевскнйБГ,СиротаАА,БеляковСЮ.柴油机加氢降低燃油消耗的研究[J].武汉水运工程学院学报,1992,16(3):253-259. 被引量:20
  • 3Vinogradov V,Kobigsky S,Petrov M.Experimental Investigation of Liquid Carbon Hydrogen Fuel Combustion in Channel at Supersonic Velocities[R].Nashville,USA:AIAA 92-3429,1992.
  • 4Andrews E H,Trexler C A,Emami S.Tests of a Fixed-Geometry Inlet-Combustor Configuration for a Hydrocarbon-Fueled Duel-Mode Scramjet[R].Indianapolis,USA:AIAA 94-2817,1994.
  • 5王艳辉,吴迪镛,迟建.氢能及制氢的应用技术现状及发展趋势[J].化工进展,2001,20(1):6-8. 被引量:74
  • 6Gurijanov E J,Harsha P T.AJAX:New directions in hypersonic technology[R].Norfolk,USA:AIAA 964609,1996.
  • 7Korabelnikov A V,Kuranov A L.High-Temperature Conversion of Liquid Hydrocarbons[R].Reno,USA:AIAA 20061442,2006.

二级参考文献7

共引文献92

同被引文献15

  • 1范学军,俞刚.大庆RP-3航空煤油热物性分析[J].推进技术,2006,27(2):187-192. 被引量:112
  • 2Vinogradov V, Kobigsky S, Petrov M. Experimental investigation of liquid carbon hydrogen fuel combustion in channel at supersonic velocities [C]//AIAA. Nashville, Tennessee, 1992, AIAA92-3429.
  • 3Andrews E H, Trexler C A, Emami S. Tests of a fixed- geometry inlet-combustor configuration for a hydrocar- bon-fueled dual-mode scramjet[C]//AIAA. Indianapolis, Indiana, 1994, AIAA-1994-2817.
  • 4Gurijanov E J, Harsha P T. AJAX: New directions in hypersonic technology [C] //AIAA. Norfolk, Virginia, 1996, AIAA-96-4609.
  • 5Korabelnikov A V, Kuranov A L. Thermal protection endothermic fuel conversion[C]//AIAA. Capua, Italy, 2005, AIAA2005-3368.
  • 6Fu Weibiao, Hou Lingyun, Zhong Beijing, et al. An analysis of the ignition of premixed gases by a hot spherical surface with catalytic reforming reaction[J]. Fuel, 2003, 80: 9-21.
  • 7Hou Lingyun, Fu Weibiao. Study on the mechanism of saving fuel-consumption for emulsified fuel with wall catalytic reforming reaction [J]. Combustion Science and Technology, 2005, 177(4): 671-689.
  • 8Hou Lingyun, Gong Jingsong, Lu Xiaofeng. Conver- sion of emulsified kerosene with catalytic reforming in a gas generator[J]. Combustion Science and Technol- ogy, 2010, 182(10): 1478-1490.
  • 9卢小丰.催化重整反应在超燃冲压发动机燃气发生器中的研究[D].北京:清华大学,2006.
  • 10侯凌云,卢小丰.小型化催化重整煤油燃气发生器的数值模拟[J].航空动力学报,2008,23(8):1359-1363. 被引量:2

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