期刊文献+

硝酸丙酯冲击点火的光谱研究 被引量:2

Spectral Studies on Shock Ignition of Propyl-nitrate
下载PDF
导出
摘要 利用从头算起法计算了硝酸丙酯分子结构,计算表明:NO2基最容易脱落。实验上利用多种光谱技术确定硝酸丙酯冲击点火延迟时间的方法是:先用谱仪确定硝酸丙酯冲击点火最早出现的中间产物,对于硝酸丙酯NO2辐射总是先出现;把单色谱仪调至NO2(463nm)波长处,并利用压力传感器测得冲击波到达样品的时间便可确定硝酸丙酯冲击点火延迟时间。这种方法比国内外常用光电二极管(峰值波长约在800nm)的方法更接近实际值。硝酸丙酯受冲击后,反应中间产物出现的时间不同,辐射强度也不同。在冲击波作用下出现的基团为NO2、O、C2、CH、CO、CO2、H2O等,而NO2基总是首先出现。采用理论和实验相结合的方法确定冲击点火延迟时间可明显减少实验量。 A molecular structure of propyl-nitrate is calculated by using ab initio calculation method. The calculation results indicate that NO2 radical is fallen away more easily. The delay time of shock ignition is determined by using the method, i.e. intermediate product of the most early emergence for the loaded propyl-nitrate is determined at first with spectrometer, the emergence of intermediate product of NO2 for propyl-nitrate after shock ignition is always the most early. The monochrometer is adjusted to 463 nm wave length of NO2 , and the time of arriving for shock wave is measured with gauge. The delay time of shock ignition for propyl-nitrate is determined. The delay time determined by the method is closer than that of by using photo-electrlc diode whose peak wave length is about 800 nm. The measurement results show that the emergence of intermediate product of O for propyl-nitrate after shock ignition is different, and radiation intensity for the radicals is also different. The emergence times for O, NO2 , CO, C2 , CH, CO2 , H2O radicals is obtained after the shock wave enters into the propyl-nitrate. The emergence time of NO2 radical is the most early. The method combined the theory with the experiment may obviously decrease tests to determine shock ignition time.
出处 《含能材料》 EI CAS CSCD 2005年第6期375-377,381,共4页 Chinese Journal of Energetic Materials
基金 国家自然科学基金资助(10172076)
关键词 物理化学 分子结构 谱仪技术 点火 冲击 physical chemistry molecular structure spectrograph technique ignition shock
  • 相关文献

参考文献2

二级参考文献7

共引文献2

同被引文献18

  • 1炎正馨,吴旌贺,胡栋,杨向东.Agglomeration Evolution of Nano-Particles Aluminium in Normal Incident Shock Wave[J].Chinese Physics Letters,2006,23(1):217-219. 被引量:2
  • 2Jones C Y, Nevers T J. Temperature-dependent distortions of the host structure of propylene oxide clathrate hy- drate[J].J Phys Chem,2010,114(9) :4194-4199.
  • 3Lifshitz A,Carmen T. isomerization and decomposition of propylene oxide studies with single-pulse shock tube [J]. J Phys Chem,1994,98(43) :1161-1173.
  • 4Yan Z X, Hu D. Shock-induced thermal behavior of aluminum nano-particles in propylene oxide [J]. J Appl Phys, 2007,249(5) :101-104.
  • 5Marinov N M, Westbrook C K, Pitz W J. Transport phenomena in combustion[J]. Combust Sci Tech, 1996,24 (3) : 118-121.
  • 6Ono R, Nifuku M, Fujiwara S, et al. Minimum ignition energy of hydrogen-air mixture: Effects of humidity and spark duration [J]. J Electrostatics, 2007,65 (2) : 87-93.
  • 7Oancea D,Razus D, Munteanu V,et al. High voltage and break spark ignition of propylene/air mixtures at various initial pressures [J].J Loss Prey Process Ind,2003,16(5) :353-361.
  • 8Kindracki J, Kobiera A, Rarat G, et al. Influence of ignition position and obstacles on explosion development in methane-air mixture in closed vessels [J]. J Loss Prev Process Ind,2007,20(4-6):551-561.
  • 9Randeberg E, Eckhoff R. Measurement of minimum ignition energies of dust clouds in the 1 mJ region[J]. J Hazard Mater, 2007,140 ( 1 ) : 237-244.
  • 10Razus D,Brinzea V, Mitu M,et al. Inerting effect of the combustion products on the confined deflagration of lique- fied petroleum gas-air mixtures [J]. J Loss Prey Process Ind, 2009,22 (4) : 463-468.

引证文献2

二级引证文献7

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