Volume 39 Issue 5
Jan.  2024
Turn off MathJax
Article Contents
ZHANG Xinwei, ZENG Wen, HU Bin, et al. Experiment on the oxidation and ignition delay characteristics of RP-3 kerosene/oxygen[J]. Journal of Aerospace Power, 2024, 39(5):20220381 doi: 10.13224/j.cnki.jasp.20220381
Citation: ZHANG Xinwei, ZENG Wen, HU Bin, et al. Experiment on the oxidation and ignition delay characteristics of RP-3 kerosene/oxygen[J]. Journal of Aerospace Power, 2024, 39(5):20220381 doi: 10.13224/j.cnki.jasp.20220381

Experiment on the oxidation and ignition delay characteristics of RP-3 kerosene/oxygen

doi: 10.13224/j.cnki.jasp.20220381
  • Received Date: 2022-05-28
    Available Online: 2023-11-02
  • The oxidation characteristics of RP-3 kerosene/O2 were experimentally tested in the flow reactor under the conditions of the equivalence ratios of 0.5, 1.0 and 2.0, the temperature range of 550−1200 K, the pressure of 0.1, 3.0 MPa. The results showed that, with the increase of equivalent ratio from 0.5 to 2.0, the starting temperature of each species formation and the corresponding temperature of the peak mole fraction of each species increased. With the increase of pressure from 0.1 MPa to 3.0 MPa, the starting temperature of each species formation and the corresponding temperature of the peak mole fraction of each species decreased, and the peak mole fraction of alkanes increased while that of alkenes decreased. Meanwhile, the ignition delay characteristics of RP-3 kerosene/O2 were experimentally tested in the shock tube under the conditions of the equivalent ratios of 0.8, and 3.5, the pressure of 0.2, 1.0, and 5.0 MPa, the temperature range of 950−1500 K. The results showed that, with the increase of the pressure and temperature or the decrease of equivalent ratio from 3.5 to 0.8, the ignition delay time of RP-3 kerosene/O2 was shortened.

     

  • loading
  • [1]
    南向谊,王拴虎,李平. 空气涡轮火箭发动机研究的进展及展望[J]. 火箭推进,2008,34(6): 31-35. NAN Xiangyi,WANG Shuanhu,LI Ping. Investigation on status and prospect of air turbine rocket[J]. Journal of Rocket Propulsion,2008,34(6): 31-35. (in Chinese

    NAN Xiangyi, WANG Shuanhu, LI Ping. Investigation on status and prospect of air turbine rocket[J]. Journal of Rocket Propulsion, 2008, 34(6): 31-35. (in Chinese)
    [2]
    THOMAS M,BOSSARD J,OSTRANDER M. Addressing emerging tactical missile propulsion challenges with the solid propellant air-turbo-rocket[R]. AIAA-2000-3309,2000.
    [3]
    THOMAS M,LEONARD A. Air-turbo-rocket combustion[R]. AIAA-95-0813,1995.
    [4]
    KAMADA T,NAKAMURA H,TEZUKA T,et al. Study on combustion and ignition characteristics of natural gas components in a micro flow reactor with a controlled temperature profile[J]. Combustion and Flame,2014,161(1): 37-48. doi: 10.1016/j.combustflame.2013.08.013
    [5]
    KACZMAREK D,HERZLER J,PORRAS S,et al. Plug-flow reactor and shock-tube study of the oxidation of very fuel-rich natural gas/DME/O2 mixtures[J]. Combustion and Flame,2021,225: 86-103. doi: 10.1016/j.combustflame.2020.10.004
    [6]
    GIMÉNEZ-LÓPEZ J,MILLERA A,BILBAO R,et al. Experimental and kinetic modeling study of the oxy-fuel oxidation of natural gas,CH4 and C2H6[J]. Fuel,2015,160: 404-412. doi: 10.1016/j.fuel.2015.07.087
    [7]
    BURKE S M,METCALFE W,HERBINET O,et al. An experimental and modeling study of propene oxidation: Part 1 speciation measurements in jet-stirred and flow reactors[J]. Combustion and Flame,2014,161(11): 2765-2784. doi: 10.1016/j.combustflame.2014.05.010
    [8]
    郑玮琳,庞历瑶,张世杰,等. 组分变化对甲烷氧化特性影响[J]. 航空动力学报,2021,36(1): 15-24. ZHENG Weilin,PANG Liyao,ZHANG Shijie,et al. Effect of composition variance on methane oxidation characteristics[J]. Journal of Aerospace Power,2021,36(1): 15-24. (in Chinese doi: 10.13224/j.cnki.jasp.2021.01.003

    ZHENG Weilin, PANG Liyao, ZHANG Shijie, et al. Effect of composition variance on methane oxidation characteristics[J]. Journal of Aerospace Power, 2021, 36(1): 15-24. (in Chinese) doi: 10.13224/j.cnki.jasp.2021.01.003
    [9]
    BURKE U,METCALFE W K,BURKE S M,et al. A detailed chemical kinetic modeling,ignition delay time and jet-stirred reactor study of methanol oxidation[J]. Combustion and Flame,2016,165: 125-136. doi: 10.1016/j.combustflame.2015.11.004
    [10]
    LIU Yuexi,RICHTER S,NAUMANN C,et al. Combustion study of a surrogate jet fuel[J]. Combustion and Flame,2019,202: 252-261. doi: 10.1016/j.combustflame.2019.01.022
    [11]
    刘靖,胡二江,黄佐华,等. RP-3航空煤油低温氧化特性的试验与数值计算[J]. 航空动力学报,2022,37(1): 36-45. LIU Jing,HU Erjiang,HUANG Zuohua,et al. Experiment and numerical calculation on low-temperature oxidation characteristics of RP-3 aviation kerosene[J]. Journal of Aerospace Power,2022,37(1): 36-45. (in Chinese doi: 10.13224/j.cnki.jasp.20210074

    LIU Jing, HU Erjiang, HUANG Zuohua, et al. Experiment and numerical calculation on low-temperature oxidation characteristics of RP-3 aviation kerosene[J]. Journal of Aerospace Power, 2022, 37(1): 36-45. (in Chinese) doi: 10.13224/j.cnki.jasp.20210074
    [12]
    ZHU Yangye,LI Sijie,DAVIDSON D F,et al. Ignition delay times of conventional and alternative fuels behind reflected shock waves[J]. Proceedings of the Combustion Institute,2015,35(1): 241-248. doi: 10.1016/j.proci.2014.05.034
    [13]
    LI Sijie,ZHU Yangye,DAVIDSON D F,et al. Pyrolysis study of conventional and alternative fuels behind reflected shock waves[J]. Fuel,2014,132: 170-177. doi: 10.1016/j.fuel.2014.04.077
    [14]
    ZHANG Jiaxiang,NIU Shaodong,ZHANG Yingjia,et al. Experimental and modeling study of the auto-ignition of n-heptane/ n-butanol mixtures[J]. Combustion and Flame,2013,160(1): 31-39. doi: 10.1016/j.combustflame.2012.09.006
    [15]
    ZHANG Yingjia,HUANG Zuohua,WEI Liangjie,et al. Experimental and modeling study on ignition delays of lean mixtures of methane,hydrogen,oxygen,and argon at elevated pressures[J]. Combustion and Flame,2012,159(3): 918-931. doi: 10.1016/j.combustflame.2011.09.010
    [16]
    ZHANG Changhua,LI Bin,RAO Fan,et al. A shock tube study of the autoignition characteristics of RP-3 jet fuel[J]. Proceedings of the Combustion Institute,2015,35(3): 3151-3158. doi: 10.1016/j.proci.2014.05.017
    [17]
    LIU Wei,QI Yunliang,ZHANG Ridong,et al. Investigation on end-gas auto-ignition and knock characteristics of iso-octane over wide thermodynamic conditions under jet ignition using a rapid compression machine[J]. Fuel,2022,313: 122665.1-122665.10.
    [18]
    LIU Wei,QI Yunliang,ZHANG Ridong,et al. Flame propagation and auto-ignition behavior of iso-octane across the negative temperature coefficient (NTC) region on a rapid compression machine[J]. Combustion and Flame,2022,235: 111688.1-111688. 12.
    [19]
    CHEN B H,LIU J Z,YAO Feng,et al. Ignition delay characteristics of RP-3 under ultra-low pressure (0.01—0.1 MPa)[J]. Combustion and Flame,2019,210: 126-133. doi: 10.1016/j.combustflame.2019.08.009
    [20]
    MAO Yebing,YU Liang,WU Zhiyong,et al. Experimental and kinetic modeling study of ignition characteristics of RP-3 kerosene over low-to-high temperature ranges in a heated rapid compression machine and a heated shock tube[J]. Combustion and Flame,2019,203: 157-169. doi: 10.1016/j.combustflame.2019.02.015
    [21]
    刘靖,胡二江,黄佐华,等. RP-3航空煤油模拟替代燃料的着火延迟特性[J]. 推进技术,2021,42(2): 467-473. LIU Jing,HU Erjiang,HUANG Zuohua,et al. Ignition delay characteristics of a surrogate fuel for RP-3 kerosene[J]. Journal of Propulsion Technology,2021,42(2): 467-473. (in Chinese doi: 10.13675/j.cnki.tjjs.190545

    LIU Jing, HU Erjiang, HUANG Zuohua, et al. Ignition delay characteristics of a surrogate fuel for RP-3 kerosene[J]. Journal of Propulsion Technology, 2021, 42(2): 467-473. (in Chinese) doi: 10.13675/j.cnki.tjjs.190545
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (45) PDF downloads(8) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return