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基于OH-PLIF技术的环形燃烧室预混火焰结构实验

王中华 唐强 张力 杨仲卿 张腾飞

王中华, 唐强, 张力, 杨仲卿, 张腾飞. 基于OH-PLIF技术的环形燃烧室预混火焰结构实验[J]. 航空动力学报, 2019, 34(9): 2010-2017. doi: 10.13224/j.cnki.jasp.2019.09.018
引用本文: 王中华, 唐强, 张力, 杨仲卿, 张腾飞. 基于OH-PLIF技术的环形燃烧室预混火焰结构实验[J]. 航空动力学报, 2019, 34(9): 2010-2017. doi: 10.13224/j.cnki.jasp.2019.09.018
Experiment on structure of premixed flame in annular combustor using OH-PLIF[J]. Journal of Aerospace Power, 2019, 34(9): 2010-2017. doi: 10.13224/j.cnki.jasp.2019.09.018
Citation: Experiment on structure of premixed flame in annular combustor using OH-PLIF[J]. Journal of Aerospace Power, 2019, 34(9): 2010-2017. doi: 10.13224/j.cnki.jasp.2019.09.018

基于OH-PLIF技术的环形燃烧室预混火焰结构实验

doi: 10.13224/j.cnki.jasp.2019.09.018
基金项目: 页岩气清洁燃烧关键技术及微型燃气轮机分布式能源系统(cstc2015shmszx90010)

Experiment on structure of premixed flame in annular combustor using OH-PLIF

  • 摘要: 针对微型燃气轮机环形燃烧室中的燃烧特性,利用平面激光诱导荧光(PLIF)技术,对环形燃烧室内甲烷/空气预混湍流多束火焰燃烧开展实验研究,得到OH自由基物质的量浓度分布,并研究雷诺数和当量比对火焰结构特征参数的影响。结果表明:OH自由基浓度分布呈现环形结构,并有火焰托举和分叉现象,OH-PLIF瞬时和平均图像揭示了火焰具有湍流和层流预混结构共同特征。火焰结构特征参数的定量分析表明,雷诺数升高,拉伸火焰预混锥形结构,促进射流之间相互作用;康达效应使内焰向内壁面弯曲,火焰张角增大;适当调节预混火焰的当量比,有利于火焰结构的稳定。

     

  • [1] CHOI M,SUNG Y,WON M,et al.Effect of fuel distribution on turbulence and combustion characteristics of a micro gas turbine combustor[J].Journal of Industrial and Engineering Chemistry,2017,48(1):24-35.
    [2] SEMPRINI S,SNCHEZ D,PASCALE A D.Performance analysis of a micro gas turbine and solar dish integrated system under different solar-only and hybrid operating conditions[J].Solar Energy,2016,132(1):279-293.
    [3] BASRAWI F,IBRAHIM T K,HABIBK,et al.Techno-economic performance of biogas-fueled micro gas turbine cogeneration systems in sewage treatment plants:Effect of prime mover generation capacity[J].Energy,2017,124(1):238-248.
    [4] 李皓然,丁天宝,李玮薇,等.某微型燃气轮机适应高原起动的技术方案[J].航空动力学报,2018,33(5):1050-1056.LI Haoran,DING Tianbao,LI Weiwei,et al.Starting technical scheme of a micro gas turbine adapting to plateau[J].Journal of Aerospace Power,2018,33 (5):1050-1056.(in Chinese)
    [5] 谢法,张珊珊,蒋洪德.入口流动参数脉动对燃气轮机燃烧室燃烧不稳定的影响[J].航空动力学报,2015,30(7):1561-1565.XIE Fa,ZHANG Shanshan,JIANG Hongde.Effects of inlet flow parameters oscillation on combustion instability of gas turbine combustor[J].Journal of Aerospace Power,2015,30(7):1561-1565.(in Chinese)
    [6] 王文波,岳明,杜春雨,等.喷嘴损伤对环形回流燃烧室性能的影响[J].航空动力学报,2017,32(6):1335-1341.WANG Wenbo,YUE Ming,DU Chunyu,et al.Effect of nozzle damage on performance of annular backflow combustor[J].Journal of Aerospace Power,2017,32(6):1335-1341.(in Chinese)
    [7] 段建东,赵克,吴凤江,等.回热循环微型燃气轮机非线性数学模型[J].航空动力学报,2014,29(1):199-206.DUAN Jiandong,ZHAO Ke,WU Fengjiang,et al.Nonlinear mathematical model of regenerative cycle micro gas turbine[J].Journal of Aerospace Power,2014,29(1):199-206.(in Chinese)
    [8] SANTIS A D,INGHAM D B,MAL,et al.CFD analysis of exhaust gas recirculation in a micro gas turbine combustor for CO2 capture[J].Fuel,2016,173(1):146-154.
    [9] 严浩,张少华,余西龙,等.OH与CH2O双组分平面激光诱导荧光对旋流燃烧室火焰结构与脉动特征的研究[J].航空动力学报,2019,34(4):894-907.YAN Hao,ZHANG Shaohua,YU Xilong,et al.Flame structure and dynamics characters investigation by OH and CH2O planar laser-induced fluorescence in the swirl combustor[J].Journal of Aerospace Power,2019,34(4):894-907.(in Chinese)
    [10] KUTNE P,MEIER W,BOXX I,et al.3 kHz PIV/OH-PLIF measurements in a gas turbine combustor at elevated pressure[J].Proceedings of the Combustion Institute,2015,35(3):3793-3802.
    [11] HBER T,GEBRETSADIK M,BOCKHORNH,et al.The effect of total reflection in PLIF imaging of annular thin films[J].International Journal of Multiphase Flow,2015,76(1):64-72.
    [12] 刘玉英,JEAN-MICHEL M,PHILIPPE B.基于氢氧基平面激光诱导荧光法的稀释燃烧机理实验研究[J].中国电机工程学报,2008,28(32):61-65.LIU Yuying,JEAN-MICHEL M,PHILIPPE B.Experimental study on dilution combustion mechanism based on hydroxyl planar laser-induced fluorescence method[J].Proceedings of the CSEE,2008,28(32):61-65.(in Chinese)
    [13] PU G,HUANG B,ZHANG X,et al.Investigation of flame structure and burning intensity of partially premixed methane enrichment of syngas using OH-PLIF and kinetic simulation[J].Combustion Theory and Modelling,2018.22(3):1-14.
    [14] LIAO Y H,HERMANSON J C.OH-PLIF Imaging of the reaction zone in swirled,strongly-pulsed jet diffusion flames with a low Reynolds number[J].Combustion Science & Technology,2017,190(4):615-631.
    [15] JIN F,TANG C,JIN W U,et al.Study on laminar flame speed and flame structure of syngas with varied compositions using OH-PLIF and spectrograph[J].International Journal of Hydrogen Energy,2013,38(3):1636-1643.
    [16] JIN F,TANG C,WU J,et al.Effect of preferential diffusion and flame stretch on flame structure and laminar burning velocity of syngas Bunsen flame using OH-PLIF[J].International Journal of Hydrogen Energy,2014,39(23):12187-12193.
    [17] YANG L,WANG Z H,ZHU Y Q,et al.Premixed jet flame characteristics of syngas using OH planar laser induced fluorescence[J].Chinese Science Bulletin,2011,56(26):2862-2868.
    [18] 张文普,丰镇平.微型燃气轮机环型燃烧室的设计研究[J].中国电机工程学报,2005,25(5):150-153.ZHANG Wenpu,FENG Zhenping.Design and research of ring combustor for micro gas turbine[J].Proceedings of the CSEE,2005,25(5):150-153 (in Chinese).
    [19] 石黎,付忠广,沈亚洲,等.值班燃料比对环形燃烧室内NOx生成影响的数值研究[J].中国电机工程学报,2016,36(22):6156-6163.SHI Li,FU Zhongguang,SHEN Yazhou,et al.Numerical simulation of pilot fuel percentage on NOx formation in an annular combustion chamber[J].Proceedings of the CSEE,2016,36(22):6156-6163.(in Chinese)
    [20] BARDIA A,SARAF R,MASLOW A,et al.The coanda effect[J].Anesthesia & Analgesia,2016,123(3):582-584.
    [21] REBA I.Applications of the coanda effect[J].Scientific American,1966,214(6):84-92.
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出版历程
  • 收稿日期:  2019-02-22
  • 刊出日期:  2019-09-28

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