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石蜡燃料的燃烧性能与其化学组成的关系
引用本文:唐乐,陈苏杭,许志伟,张伟,沈瑞琪,叶迎华.石蜡燃料的燃烧性能与其化学组成的关系[J].含能材料,2017,25(8):633-638.
作者姓名:唐乐  陈苏杭  许志伟  张伟  沈瑞琪  叶迎华
作者单位:南京理工大学化工学院,江苏南京,210094
基金项目:工信部自主科研专项基金资助
摘    要:为了研究石蜡的燃烧性能与其化学组成之间的关系,针对54~#、58~#、62~#和66~#4种粗晶石蜡开展了气相色谱分析,并测试了4种石蜡的燃烧热和在氧气流中的瞬时退移速率,同时利用N ASA-C EA软件计算了4种石蜡燃料不同氧燃比下的能量特性。结果表明:54~#、58~#、62~#和66~#4种粗晶石蜡的平均分子式分别为C_(26.40)H_(54.80)、C_(27.59)H_(57.18)、C_(28.02)H_(58.04)和C_(32.11)H_(66.22),正构烷烃含量分别为92.79%、89.44%、88.36%和84.55%;平均碳数n越大、正构烷烃含量越小的石蜡其燃烧热越低;随着平均碳数n值的增大以及正构烷烃含量的降低,石蜡的退移速率降低。NASA-CEA程序计算得到4种石蜡的能量特性受其化学组成的影响很小,其最佳氧燃比均为2.7,对应的理论比冲约为354 s,绝热火焰温度约为3600 K。

关 键 词:固液混合发动机  石蜡燃料  气相色谱  化学组成  燃烧热  退移速率  能量特性
收稿时间:2017/2/15 0:00:00
修稿时间:2017/3/22 0:00:00

Relationship between Combustion Characteristics and Chemical Components of Paraffin Fuel
TANG Yue,CHEN Su-hang,XU Zhi-wei,ZHANG Wei,SHEN Rui-qi and YE Ying-hua.Relationship between Combustion Characteristics and Chemical Components of Paraffin Fuel[J].Chinese Journal of Energetic Materials,2017,25(8):633-638.
Authors:TANG Yue  CHEN Su-hang  XU Zhi-wei  ZHANG Wei  SHEN Rui-qi and YE Ying-hua
Affiliation:School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China,School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China,School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China,School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China,School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China and School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing, 210094, China
Abstract:Paraffin fuels are ideal energy for hybrid rocket engine owing to the characteristics of high regression rate.In order to study the relationship between the combustion characteristics and chemical components of paraffin fuel,the gas chromatography was carried out for 54#,58#,62# and 66# 4 kinds of macrocrystalline paraffin fuels,and measured the combustion heat and the regression rate in the oxygen flow rate of these 4 kinds of macrocrystalline paraffin fuels.In addition,the energy characteristics of these macro-crystalline paraffin fuels at different oxygen fuel ratio were calculated using NASA-CEA software.The results show that the average molecular formulas of the 54#,58#,62# and 66#4 kinds of macrocrystalline paraffin were C26.40 H54.80,C27.59H57.18,C28.02 H58.04 and C32.11H66.22,respectively,and the percentage contents of the n-alkanes of the 54#,58#,62# and 66# 4 kinds of macrocrystalline paraffin were 92.79%,89.44%,88.36% and 84.55%,respectively.The bigger the carbon number as well as the less the percentage content of n-alkanes,the smaller the combustion heat of paraffin fuel.And the regression rates of paraffin fuels were reduced along with the increase of carbon number.According to the calculated results of NASA-CEA software,the theoretical specific impulse of paraffin fuels were decreased with the carbon number of paraffin increasing,and the adiabatic flame temperatures were increased with the carbon number of paraffin increasing,but these influences of the chemical components of paraffin fuels on the energy characteristics were insignificant.The optimum oxygen fuel ratio of 4 kinds of macrocrystalline paraffin were all 2.7,the theoretical specific impulse were all about 354 s more than HTPB,and the adiabatic flame temperature were all about 3600 K less than HTPB.
Keywords:hybrid rocket engine  paraffin fuel  gas chromatography  chemical components  combustion heat  regression rate  energy characteristics
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