Volume 40 Issue 4
Apr.  2025
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2025  >  40(4): 20220815
MIAO Junjie, LI Xiankai, YIN Chao, et al. Effect of evaporation chamber structure on flow characteristics and flame development mechanisms of V-gutter flameholder[J]. Journal of Aerospace Power, 2025, 40（4）：20220815 doi: 10.13224/j.cnki.jasp.20220815
Citation: MIAO Junjie, LI Xiankai, YIN Chao, et al. Effect of evaporation chamber structure on flow characteristics and flame development mechanisms of V-gutter flameholder[J]. Journal of Aerospace Power, 2025, 40（4）：20220815 doi: 10.13224/j.cnki.jasp.20220815
shu

Effect of evaporation chamber structure on flow characteristics and flame development mechanisms of V-gutter flameholder

doi: 10.13224/j.cnki.jasp.20220815
  • 1.

    College of Energy and Power Engineering，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China

  • 2.

    Yangzhou Collaborative Innovation Research Institute Company Limited，Shenyang Aircraft Design and Research Institute，Aviation Industry Corporation of China，Limited，Yangzhou Jiangsu 225111，China

  • Received Date: 2022-10-24
    Available Online: 2024-12-13
    Abstract

  • The effect of evaporation chamber structure on flow characteristics and flame development mechanisms of a novel evaporating V-gutter flameholder at Ma=0.15—0.35 and 320 K was studied by numerical simulation and experimental methods, and the flame stabilization mechanisms at lean and rich states were revealed. The effects of the structural parameters of the evaporation chamber, such as the intake area and the ratio of evaporation holes’ area to the intake area, on the performance of lean ignition and blowout were summarized. The results showed that the flame quenching caused by flame instability during ignition was similar to that at rich state, due to the enhanced fuel accumulation caused by ignition transience. Rising the ratio of evaporation holes’ area to the intake area can expand the pilot recirculation zone and enhance the flame stability, but it may weaken the fuel atomization and reduce the chemical reaction rate, resulting in a slower flame development and a lower flame intensity. Increasing the intake area can simultaneously expand the pilot recirculation zone and improve the fuel atomization, thereby accelerating the flame development and promoting the transition towards the flame stabilization mechanism at lean state, making it more conducive to improving the lean ignition and flame-holding performance of the evaporating V-gutter flameholder.

     

    • FullText(HTML)
  • loading
    • References(21)
  • [1]
    刘大响,金捷. 21世纪世界航空动力技术发展趋势与展望[J]. 中国工程科学,2004,6(9): 1-8. LIU Daxiang,JIN Jie. The development trends and prospect of world aeropropulsion technology in the 21st century[J]. Engineering Science,2004,6(9): 1-8. (in Chinese

    LIU Daxiang, JIN Jie. The development trends and prospect of world aeropropulsion technology in the 21st century[J]. Engineering Science, 2004, 6(9): 1-8. (in Chinese)
    [2]
    SZIROCZAK D,SMITH H. A review of design issues specific to hypersonic flight vehicles[J]. Progress in Aerospace Sciences,2016,84: 1-28. doi: 10.1016/j.paerosci.2016.04.001
    [3]
    SERBIN S I,MATVEEV I B,MOSTIPANENKO G B. Investigations of the working process in a “lean-burn” gas turbine combustor with plasma assistance[J]. IEEE Transactions on Plasma Science,2011,39(12): 3331-3335. doi: 10.1109/TPS.2011.2166811
    [4]
    WILLIAM R R. Experimental investigations into high-altitude relight of a gas turbine[D]. Cambridge,East of England,UK: University of Cambridge,2008.
    [5]
    朱志新,何小民,宋耀宇,等. 基于蒸发式值班稳焰的涡轮基组合燃烧室燃烧性能研究[J]. 推进技术,2016,37(4): 698-705. ZHU Zhixin,HE Xiaomin,SONG Yaoyu,et al. Experimental investigations on combustion characteristics of a vaporized-flameholder pilot combustor in TBCC engine[J]. Journal of Propulsion Technology,2016,37(4): 698-705. (in Chinese

    ZHU Zhixin, HE Xiaomin, SONG Yaoyu, et al. Experimental investigations on combustion characteristics of a vaporized-flameholder pilot combustor in TBCC engine[J]. Journal of Propulsion Technology, 2016, 37(4): 698-705. (in Chinese)
    [6]
    马文杰. 吸气式一体化喷油稳定器流动和燃烧性能研究[D]. 北京: 北京航空航天大学,2008. MA Wenjie. Study on flow and combustion performance of air-breathing integrated fuel injection flameholder[D]. Beijing: Beijing University of Aeronautics and Astronautics,2006. (in Chinese

    MA Wenjie. Study on flow and combustion performance of air-breathing integrated fuel injection flameholder[D]. Beijing: Beijing University of Aeronautics and Astronautics, 2006. (in Chinese)
    [7]
    高昭. 蒸发式火焰稳定器点火性能研究[D]. 北京: 北京航空航天大学,2016. GAO Zhao. Study on ignition performance of piloted vaporization flameholder[D]. Beijing: Beijing University of Aeronautics and Astronautics,2006. (in Chinese

    GAO Zhao. Study on ignition performance of piloted vaporization flameholder[D]. Beijing: Beijing University of Aeronautics and Astronautics, 2006. (in Chinese)
    [8]
    程晓军,范育新,王家骅. 薄膜蒸发稳定器在超级燃烧室内贫油点熄火特性[J]. 推进技术,2015,36(2): 246-252. CHENG Xiaojun,FAN Yuxin,WANG Jiahua. Performances of lean ignition and lean blowout with film evaporation flameholder in hyperburner[J]. Journal of Propulsion Technology,2015,36(2): 246-252. (in Chinese

    CHENG Xiaojun, FAN Yuxin, WANG Jiahua. Performances of lean ignition and lean blowout with film evaporation flameholder in hyperburner[J]. Journal of Propulsion Technology, 2015, 36(2): 246-252. (in Chinese)
    [9]
    朱志新,何小民,薛冲,等. 涡轮基组合循环发动机超级燃烧室燃烧性能试验[J]. 航空动力学报,2015,30(9): 2115-2121. ZHU Zhixin,HE Xiaomin,XUE Chong,et al. Experiment on performance of a hyper-combustor utilized in turbine based combined cycle engine[J]. Journal of Aerospace Power,2015,30(9): 2115-2121. (in Chinese

    ZHU Zhixin, HE Xiaomin, XUE Chong, et al. Experiment on performance of a hyper-combustor utilized in turbine based combined cycle engine[J]. Journal of Aerospace Power, 2015, 30(9): 2115-2121. (in Chinese)
    [10]
    刘鸿,王方,王家骅. 特种V型蒸发式火焰稳定器的低压性能试验研究[J]. 江苏工业学院学报,2004,16(1): 12-14. LIU Hong,WANG Fang,WANG Jiahua. Experimental study of the performance of special evaporating V-gutter flame-holder at low pressure[J]. Journal of Changzhou University (Natural Science Edition),2004,16(1): 12-14. (in Chinese

    LIU Hong, WANG Fang, WANG Jiahua. Experimental study of the performance of special evaporating V-gutter flame-holder at low pressure[J]. Journal of Changzhou University (Natural Science Edition), 2004, 16(1): 12-14. (in Chinese)
    [11]
    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): 2753-2760. 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): 2753-2760. (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): 2753-2760. (in Chinese)
    [12]
    金莉,谭永华. 蒸发式火焰稳定器冷态流场计算[J]. 火箭推进,2007,33(1): 23-27. JIN Li,TAN Yonghua. Numerical prediction of cold flow field behind a vapor flameholder[J]. Journal of Rocket Propulsion,2007,33(1): 23-27. (in Chinese

    JIN Li, TAN Yonghua. Numerical prediction of cold flow field behind a vapor flameholder[J]. Journal of Rocket Propulsion, 2007, 33(1): 23-27. (in Chinese)
    [13]
    韩启祥,王家骅. 沙丘驻涡蒸发式稳定器低压性能的试验研究[J]. 推进技术,2001,22(1): 40-42,76. HAN Qixiang,WANG Jiahua. Experimental investigation on performance of vapor barchane dune vortex flame-holder at low pressure[J]. Journal of Propulsion Technology,2001,22(1): 40-42,76. (in Chinese

    HAN Qixiang, WANG Jiahua. Experimental investigation on performance of vapor barchane dune vortex flame-holder at low pressure[J]. Journal of Propulsion Technology, 2001, 22(1): 40-42, 76. (in Chinese)
    [14]
    郑殿峰,张会强,林文漪,等. 蒸发式稳定器常压和低压燃烧性能试验研究[J]. 哈尔滨工业大学学报,2004,36(12): 1724-1728. ZHENG Dianfeng,ZHANG Huiqiang,LIN Wenyi,et al. Experimental investigation on performance of vapor flame holder at normal and low pressure[J]. Journal of Harbin Institute of Technology,2004,36(12): 1724-1728. (in Chinese doi: 10.3321/j.issn:0367-6234.2004.12.039

    ZHENG Dianfeng, ZHANG Huiqiang, LIN Wenyi, et al. Experimental investigation on performance of vapor flame holder at normal and low pressure[J]. Journal of Harbin Institute of Technology, 2004, 36(12): 1724-1728. (in Chinese) doi: 10.3321/j.issn:0367-6234.2004.12.039
    [15]
    郑殿峰,张会强,林文漪,等. 蒸发式稳定器气态燃料掺混特性和蒸发管的流量系数[J]. 燃烧科学与技术,2004,10(1): 28-31. ZHENG Dianfeng,ZHANG Huiqiang,LIN Wenyi,et al. Mixing characteristics of gaseous fuel in vapor flame holder and discharge coefficient of evaporating pipe[J]. Journal of Combustion Science and Technology,2004,10(1): 28-31. (in Chinese doi: 10.3321/j.issn:1006-8740.2004.01.006

    ZHENG Dianfeng, ZHANG Huiqiang, LIN Wenyi, et al. Mixing characteristics of gaseous fuel in vapor flame holder and discharge coefficient of evaporating pipe[J]. Journal of Combustion Science and Technology, 2004, 10(1): 28-31. (in Chinese) doi: 10.3321/j.issn:1006-8740.2004.01.006
    [16]
    CHENG Xiaojun,FAN Yuxin. Experimental study of lean ignition and lean blowout performance improvement using an evaporation flameholder[J]. International Journal of Heat and Mass Transfer,2016,103: 319-326. doi: 10.1016/j.ijheatmasstransfer.2016.07.003
    [17]
    航空发动机设计手册编委. 航空发动机设计手册:第十一分册[M]. 北京: 航空工业出版社,2000.
    [18]
    SIMMONS M J H,HANRATTY T J. Droplet size measurements in horizontal annular gas-liquid flow[J]. International Journal of Multiphase Flow,2001,27(5): 861-883. doi: 10.1016/S0301-9322(00)00053-7
    [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]
    MIAO Junjie,FAN Yuxin,LIU Tianchi,et al. Experimental and numerical study on thermodynamic characteristics in a Z-shaped evaporating pilot-flameholder[J]. Acta Astronautica,2019,162: 56-65. doi: 10.1016/j.actaastro.2019.05.036
    [21]
    MASTORAKOS E. Forced ignition of turbulent spray flames[J]. Proceedings of the Combustion Institute,2017,36(2): 2367-2383. doi: 10.1016/j.proci.2016.08.044
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF(4168.0KB)
    XML

    Article Metrics

    Article views (479) PDF downloads(32) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return