Volume 40 Issue 2
Feb.  2025
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GAO Tianhua, LIU Yong, DENG Zijiang, et al. Investigation on ignition performance prediction model of typical model afterburner[J]. Journal of Aerospace Power, 2025, 40(2):20220315 doi: 10.13224/j.cnki.jasp.20220315
Citation: GAO Tianhua, LIU Yong, DENG Zijiang, et al. Investigation on ignition performance prediction model of typical model afterburner[J]. Journal of Aerospace Power, 2025, 40(2):20220315 doi: 10.13224/j.cnki.jasp.20220315

Investigation on ignition performance prediction model of typical model afterburner

doi: 10.13224/j.cnki.jasp.20220315
Funds:  National Science and Technology Major Project (2017-Ⅲ-0007-0033)
  • Received Date: 2022-05-09
    Available Online: 2024-10-18
  • Based on the experiments and numerical simulation, the prediction models of lean oil ignition for three kinds of afterburner with evaporative slot, cavity and cavity strut were established. According to the Lefebvre semi-empirical ignition model, the comprehensive influence mechanism of inlet temperature, pressure and flow rate on fuel atomization and depleted fuel ignition boundary was analyzed. The semi-empirical model of fuel particle size was replaced, and a fully empirical ignition prediction model based on inlet boundary was formed. The model can explicitly reflect the favorable and unfavorable action mechanisms of inlet flow on ignition, and the error of prediction and experiment data of lean oil ignition boundary of the three combustion chamber models was less than 10%. The model method could provide a reference for the establishment of a prediction model for lean oil ignition in engineering afterburner.

     

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  • [1]
    张宝诚. 航空发动机燃烧室的现状和发展[J]. 航空发动机,2013,39(6): 67-73. ZHANG Baocheng. Status and development of aeroengine combustors[J]. Aeroengine,2013,39(6): 67-73. (in Chinese

    ZHANG Baocheng. Status and development of aeroengine combustors[J]. Aeroengine, 2013, 39(6): 67-73. (in Chinese)
    [2]
    张孝春,孙雨超,刘涛. 先进加力燃烧室设计技术综述[J]. 航空发动机,2014,40(2): 24-30,60. ZHANG Xiaochun,SUN Yuchao,LIU Tao. Summary of advanced afterburner design technology[J]. Aeroengine,2014,40(2): 24-30,60. (in Chinese

    ZHANG Xiaochun, SUN Yuchao, LIU Tao. Summary of advanced afterburner design technology[J]. Aeroengine, 2014, 40(2): 24-30, 60. (in Chinese)
    [3]
    谭云川,钟华贵,孙瑞礼,等. 驻涡加力燃烧室贫油熄火性能的影响[J]. 航空动力学报,2021,36(9): 1932-1941. TAN Yunchuan,ZHONG Huagui,SUN Ruili,et al. Effect of lean blowout performance of trapped vortex combustor of the afterburner[J]. Journal of Aerospace Power,2021,36(9): 1932-1941. (in Chinese

    TAN Yunchuan, ZHONG Huagui, SUN Ruili, et al. Effect of lean blowout performance of trapped vortex combustor of the afterburner[J]. Journal of Aerospace Power, 2021, 36(9): 1932-1941. (in Chinese)
    [4]
    刘冉,刘玉英,高昭. 结构参数对蒸发式火焰稳定器贫油熄火性能的影响及其预测方法研究[J]. 推进技术,2017,38(12): 119-110. LIU Ran,LIU Yuying,GAO Zhao. Structural parameters effects on lean blowout performance and prediction method for piloted vaporization flameholder [J]. Journal of Propulsion Technology,2017,38(12):31-35. (in Chinese

    LIU Ran, LIU Yuying, GAO Zhao. Structural parameters effects on lean blowout performance and prediction method for piloted vaporization flameholder [J]. Journal of Propulsion Technology, 2017, 38(12): 31-35. (in Chinese)
    [5]
    金捷,吴迪,季鹤鸣. 带凹腔的支板火焰稳定装置及火焰稳定方法. CN102200292A[P]. 2011-09-28.
    [6]
    刘雯佳,金捷,季鹤鸣. 凹腔支板火焰稳定器冷态流场对点火特性影响规律的数值模拟分析[J]. 燃气涡轮试验与研究,2010,23(4): 35-38. LIU Wenjia,JIN Jie,JI Heming. Numerical simulation analysis of a cavity strut flame stabilizer cold flow field influence on ignition characteristics[J]. Gas Turbine of Experiments and Research,2010,23(4): 35-38. (in Chinese

    LIU Wenjia, JIN Jie, JI Heming. Numerical simulation analysis of a cavity strut flame stabilizer cold flow field influence on ignition characteristics[J]. Gas Turbine of Experiments and Research, 2010, 23(4): 35-38. (in Chinese)
    [7]
    HSU K,GROSS L,TRUMP D,et al. Performance of a trapped-vortex combustor[R]. Washington DC: American Institute of Aeronautics and Astronautics,2004.
    [8]
    桂韬,房人麟,邱伟,等. 同轴分区高温升燃烧室点火性能试验研究[J]. 推进技术,2022,43(3): 216-224. GUI Tao,FANG Renlin,QIU Wei,et al. Experimental investigation on ignition performance of coaxial and divisional high temperature rise combustor[J]. Journal of Propulsion Technology,2022,43(3): 216-224. (in Chinese

    GUI Tao, FANG Renlin, QIU Wei, et al. Experimental investigation on ignition performance of coaxial and divisional high temperature rise combustor[J]. Journal of Propulsion Technology, 2022, 43(3): 216-224. (in Chinese)
    [9]
    LEFEBVRE A H. Ignition theory and its application to the altitude relighting performance of gas turbine combustors[C]//Combustion and Heat Transfer in Gas Turbine Systems. Amsterdam: Elsevier,1971: 105-116.
    [10]
    TAYLOR J R,WIDENER S. Altitude ignition/lean deceleration study[R]. Washington DC: American Institute of Aeronautics and Astronautics,1986.
    [11]
    FOUST M,THOMSEN D,STICKLES R,et al. Development of the GE aviation low emissions TAPS combustor for next generation aircraft engines[R]. Washington DC: American Institute of Aeronautics and Astronautics ,2012.
    [12]
    史家荣. 短环燃烧室点火和燃烧稳定性能研究[C]//中国航空学会青年科技论坛论文集. 北京: 中国航空学会,2004: 268-273. SHI Jiarong. Study on ignition and combustion stability of short-ring combustion chamber[C]//Proceedings of the Youth Science and Technology Forum of China Aviation Society. Beijing: China aviation society,2004: 268-273. (in Chinese

    SHI Jiarong. Study on ignition and combustion stability of short-ring combustion chamber[C]//Proceedings of the Youth Science and Technology Forum of China Aviation Society. Beijing: China aviation society, 2004: 268-273. (in Chinese)
    [13]
    黄夏,王慧汝. 凹腔支板火焰稳定器冷态流场对点火特性影响规律的数值模拟分析[J]. 燃气涡轮试验与研究,2018,31(5): 11-16,62. HUANG Xia,WANG Huiru. Numerical simulation analysis of the influence of cavity-supported flame stabilizer on ignition characteristics[J]. Gas Turbine Experiment and Research,2018,31(5): 11-16,62. (in Chinese

    HUANG Xia, WANG Huiru. Numerical simulation analysis of the influence of cavity-supported flame stabilizer on ignition characteristics[J]. Gas Turbine Experiment and Research, 2018, 31(5): 11-16, 62. (in Chinese)
    [14]
    王延胜,林宇震,李林,等. 中心分级燃烧室点火性能试验研究[J]. 推进技术,2016,37(1): 98-104. WANG Yansheng,LIN Yuzhen,LI Lin,et al. Experimental investigation on ignition performance of internally-staged combustor[J]. Journal of Propulsion Technology,2016,37(1): 98-104. (in Chinese

    WANG Yansheng, LIN Yuzhen, LI Lin, et al. Experimental investigation on ignition performance of internally-staged combustor[J]. Journal of Propulsion Technology, 2016, 37(1): 98-104. (in Chinese)
    [15]
    王凯兴. 燃烧室高空低温低压点火试验及数值模拟研究 [R]. 北京: 中国科学院工程热物理研究所,2021.
    [16]
    缪俊杰,范育新,吴伟秋,等. 蒸发式Z形值班火焰稳定器的点火性能[J]. 航空动力学报,2020,35(7): 1457-1465. MIAO Junjie,FAN Yuxin,WU Weiqiu,et al. Ignition characteristics in evaporating Z-shaped pilot flame-holder[J]. Journal of Aerospace Power,2020,35(7): 1457-1465. (in Chinese

    MIAO Junjie, FAN Yuxin, WU Weiqiu, et al. Ignition characteristics in evaporating Z-shaped pilot flame-holder[J]. Journal of Aerospace Power, 2020, 35(7): 1457-1465. (in Chinese)
    [17]
    冯玉桦,刘玉英,邓远灏,等. 含湿量对蒸发式火焰稳定器贫油熄火性能的影响[J]. 航空动力学报,2020,35(9): 1866-1874. FENG Yuhua,LIU Yuying,DENG Yuanhao,et al. Effects of humidity ratio on lean blowout performance of piloted vaporization flameholder[J]. Journal of Aerospace Power,2020,35(9): 1866-1874. (in Chinese

    FENG Yuhua, LIU Yuying, DENG Yuanhao, et al. Effects of humidity ratio on lean blowout performance of piloted vaporization flameholder[J]. Journal of Aerospace Power, 2020, 35(9): 1866-1874. (in Chinese)
    [18]
    陈亮任,凌文辉. 低压下蒸发式稳定器结构对燃烧效率的影响[J]. 战术导弹技术,2013(6): 66-73. CHEN Liangren,LING Wenhui. Influence of vaporizing flame holder structure on combustion efficiency at low pressure[J]. Tactical Missile Technology,2013(6): 66-73. (in Chinese

    CHEN Liangren, LING Wenhui. Influence of vaporizing flame holder structure on combustion efficiency at low pressure[J]. Tactical Missile Technology, 2013(6): 66-73. (in Chinese)
    [19]
    MIAO Junjie,FAN Yuxin,WU Weiqiu,et al. Effect of preheated fuel supply by gas reflux on thermodynamic characteristics in a cavity-based integrated combustor[J]. Aerospace Science and Technology,2021,108: 106352. doi: 10.1016/j.ast.2020.106352
    [20]
    HUANG Yakun,HE Xiaomin,ZHANG Huangwei,et al. Flame stability optimization of cavity primary air-jet form in an augmentor[J]. Energy,2022,239: 121801. doi: 10.1016/j.energy.2021.121801
    [21]
    HUANG Yakun,HE Xiaomin,ZHU Zhixin,et al. Inlet pressure effects on subatmospheric flame stabilization with an optimum size of a cavity-based combustor[J]. International Journal of Aerospace Engineering,2020,2020: 4126753.
    [22]
    MIAO Junjie,FAN Yuxin,LIU Tianchi. Influence of strut on cavity at subsonic speeds: ignition characteristics[J]. Proceedings of the Institution of Mechanical Engineers:Part G Journal of Aerospace Engineering,2020,234(8): 1369-1379. doi: 10.1177/0954410020904832
    [23]
    LEFEBVRE A H. BALLAL D R. Gas turbine combustion: alternative fuels and emissions[J]. Journal Engineering for Gas Turbines and Power,2010,132(11): 116501. doi: 10.1115/1.4001927
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