期刊文献+

液体推进剂液滴电点火特性的实验研究 被引量:5

Experimental Study on Electrical Ignition Properties of Liquid Propellant Droplet
下载PDF
导出
摘要 为了研究HAN基液体推进剂电点火特性,设计了液体推进剂液滴低压电加热点火模拟试验装置,利用高速录像系统,观测了HAN基液体推进剂LP1846单滴在不同电加热速率下的点火特性,结果表明,LP1846液滴在通电时主要经历四个特征过程,即:蒸发过程、周期性膨胀收缩过程、热分解过程和着火燃烧过程,且在膨胀收缩过程中伴有微爆现象发生。电压加载速率从80 V.s-1增大到140 V.s-1过程中,液滴着火延迟期从0.82 s变为0.62 s,呈线性缩短,且着火时火焰越明亮。 In order to study the electrical ignition properties of HAN-based liquid propellant, an experimental device of electrical heating ignition of liquid propellant droplet was designed. By using high speed camera system, the ignition properties of LP1846 single droplet was observed at different electrical heating rates. The results show that when the LP1846 droplet is electrified,it goes mainly through four characteristic processes,i, e. evaporization process,periodic expansion and contraction process,stronger thermal decomposition process,and ignition and combustion process. When peak load voltage is from 80 V·s^-1 to 140 V·s^-1 ,the ignition delay time of LP1846 droplet is linearly shorten from 0. 82 s to 0.62 s,but the flame is lighter.
出处 《含能材料》 EI CAS CSCD 2008年第5期625-628,共4页 Chinese Journal of Energetic Materials
基金 国家自然科学基金(50776048)
关键词 燃烧学 液体推进剂 电点火 瞬态测量 combustion liquid propellant electrical ignition transient measurement
  • 相关文献

参考文献14

  • 1Law C K. Ignition and combustion of liquid propellants [ R ]. ADA224150,1990.
  • 2Lee H S,Litzinger T C. Thermal decomposition of HAN-based liquid propellants[ J]. Combustion and Flame,2001,123 : 2205 - 2222.
  • 3Chang Y P,Bayer E, Kuo K K. Combustion behavior and flame struc-ture of XM46 liquid propellant[ J]. Journal of Propulsion and power, 2001,17(4) ,. 800 -808.
  • 4余永刚,金志明,曾毓敏.HAN基液滴在富含水蒸气环境中着火、燃烧特性研究[J].兵工学报,2001,22(3):289-292. 被引量:5
  • 5Meinhardt D S. Development and testing of new,HAN-based monopro-pellants in small rocket thrusters[ R]. AIAA-1998-4006,1998.
  • 6Bombelli V,Simon D. Economic benefits of the use of non-toxic mono-propellants for spacecraft applications[R]. AIAA-2003-4783,2003.
  • 7Yetter R A, Yang V, Wang Z,et al. Development of meso and micro scale liquid propellant thrusters[R]. AIAA-2003-0676,2003.
  • 8DeSpirito J, Knapton J D. Electrical ignition of HAN-baaed liquid propellants[ R]. ADA195094,1988.
  • 9Klingenberg G,Frieske H J. Electrical Ignition of HAN-based liquid propellants[R]. ADA223272,1990.
  • 10Klingenberg G, Rockstroh H, Knapton J D, et al. Investigation of liquid gun propellants: Electrical ignition of LGP1846 [J]. Journal of Propellants, Explosives, Pyrotechnics, 1990,15 ( 3 ) : 103 - 114.

二级参考文献3

共引文献5

同被引文献44

  • 1余永刚,金志明.含能液滴在对流环境中着火燃烧特性研究[J].推进技术,1996,17(2):53-58. 被引量:2
  • 2禹天福.空间化学推进技术的发展[J].火箭推进,2005,31(6):23-29. 被引量:6
  • 3贺芳,方涛,李亚裕,米镇涛.新型绿色液体推进剂研究进展[J].火炸药学报,2006,29(4):54-57. 被引量:35
  • 4任晓光,李明慧,王爱琴,李林,王晓东,张涛.室温条件下硝酸羟胺的催化分解[J].催化学报,2007,28(1):1-2. 被引量:4
  • 5Hurbert E, Applenhite J. Nontoxic Orbital Maneuvering and Reaction Control Systems for Reusable Spacecraft [J]. Journal of Propulsion and Power, 1998, 14(5): 676-687.
  • 6Meinhardt D S. Development and Testing of New, HAN- Based Monopropellants in Small Rocket Thrusers [R]. AIAA-1998-4006, Alexander: U.S. AIAA, 1998.
  • 7Anflo K. Development and Testing of AND-Based Monopropellants in Small Rocket Engines [R]. AIAA-2000-3162, Alexander: U. S. AIAA, 2000.
  • 8Chang Y P, Boyer E, Kuo K K. Combustion Behavior and Flame Structure of XM46 Liquid Propellants [J]. Journal of Propulsion and Power, 2001, 17(4): 800-808.
  • 9Farshchi M, Vaezi V, Shaw B D. Studies of HAN-Based Monopropellant Droplet Combustion [J]. Combust. Sci. and Tech., 2002, 174(7): 71-97.
  • 10Yetter R A, Yang V, et al. Development of Meso and Micro Scale Liquid Propellant Thrusters [R]. AIAA-2003- 0676, Alexander: U. S. AIAA, 2003.

引证文献5

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部