留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

高温来流下U型脉冲爆震燃烧室燃烧特性试验

谭汶昊 郑龙席 卢杰 王凌羿 黄康

谭汶昊, 郑龙席, 卢杰, 王凌羿, 黄康. 高温来流下U型脉冲爆震燃烧室燃烧特性试验[J]. 航空动力学报, 2022, 37(3): 502-510. doi: 10.13224/j.cnki.jasp.20210159
引用本文: 谭汶昊, 郑龙席, 卢杰, 王凌羿, 黄康. 高温来流下U型脉冲爆震燃烧室燃烧特性试验[J]. 航空动力学报, 2022, 37(3): 502-510. doi: 10.13224/j.cnki.jasp.20210159
TAN Wenhao, ZHENG Longxi, LU Jie, WANG Lingyi, HUANG Kang. Experiment on combustion characteristics of U-bend pulse detonation combustor under high temperature inlet stream[J]. Journal of Aerospace Power, 2022, 37(3): 502-510. doi: 10.13224/j.cnki.jasp.20210159
Citation: TAN Wenhao, ZHENG Longxi, LU Jie, WANG Lingyi, HUANG Kang. Experiment on combustion characteristics of U-bend pulse detonation combustor under high temperature inlet stream[J]. Journal of Aerospace Power, 2022, 37(3): 502-510. doi: 10.13224/j.cnki.jasp.20210159

高温来流下U型脉冲爆震燃烧室燃烧特性试验

doi: 10.13224/j.cnki.jasp.20210159
基金项目: 中央高校基本科研业务费专项资金(G2021KY05114); 中国空气动力研究与发展中心基础和前沿技术研究基金(PJD20170145)
详细信息
    作者简介:

    谭汶昊(1995-),男,博士生,主要从事脉冲爆震涡轮发动机控制研究。

    通讯作者:

    卢杰(1988-),男,副教授,博士,主要从事爆震燃烧与爆震推进研究。E-mail:lujie@nwpu.edu.cn

  • 中图分类号: V231.2

Experiment on combustion characteristics of U-bend pulse detonation combustor under high temperature inlet stream

  • 摘要: 为了获得高温来流下气/液两相多循环U型脉冲爆震燃烧室(U-PDC)的燃烧特性,使用汽油/空气为燃料和氧化剂开展了相关试验研究。结果表明:当来流温度为373 K,U-PDC能够在15~38 Hz范围内稳定工作,且随着工作频率提高爆燃向爆震转变(DDT)距离缩短;在室温条件下、工作频率为15~25 Hz时,未能形成充分发展爆震波,表明高温来流可促进DDT过程。在室温条件下、工作频率为15~25 Hz时,由于U型爆震弯段内可燃混气分布不均匀,U型爆震弯段外侧监测到火焰的时间晚于U型弯段出口,当来流温度升至373 K后该现象明显改善。此外,U-PDC的点火起爆时间在3~10 ms内,且点火延迟时间是影响点火起爆时间的主要因素;U-PDC工作频率相同、来流温度从室温升高至373 K或来流温度相同、U-PDC工作频率提高时,波速随之提高,点火起爆时间缩短。

     

  • [1] 严传俊,范玮,郑龙席,等.脉冲爆震发动机原理及关键技术[M].西安:西北工业大学出版社,2005.
    [2] 郑龙席,王治武,黄希桥,等.脉冲爆震涡轮发动机技术[M].西安:西北工业大学出版社,2019.
    [3] 郑龙席,卢杰,严传俊,等.脉冲爆震涡轮发动机研究进展[J].航空动力学报,2014,29(5):993-1000.
    [4] 李晓丰,郑龙席,邱华,等.两相脉冲爆震涡轮发动机原理性试验[J].航空动力学报,2013,28(12):2731-2736.
    [5] KAILASANATH K.Recent developments in the research on pulse detonation engines[J].AIAA Journal,2003,41(2):145-159.
    [6] 王凌羿,郑龙席,黄康,等.回流型脉冲爆震燃烧室工作特性分析[J].推进技术,2021,42(4):898-905.
    [7] JEFFREY G,VENKAT T,ANTHONY D.System-level performance estimation of a pulse detonation based hybrid engine[J].Journal of Engineering for Gas Turbine and Power 2008,130(1):1-8.
    [8] LI Xiaofeng,ZHENG Longxi,QIU Hua,et al.Experimental investigation on the power extraction of a turbine driven by a pulse detonation combustor[J].Chinese Journal of Aeronautics,2013,26(6):1353-1359.
    [9] WILLIAM H H,DAVID T P.Thermodynamic cycle analysis of pulse detonation engines[J].Journal of Propulsion and Power ,2002,18(1):68-76.
    [10] HELFRICH T M,SCHAUER F R.Ignition and detonation-initiation characteristics of hydrogen and hydrocarbon fuels in a PDE[R].Reno,US:the 45th AIAA Aerospace Sciences Meeting and Exhibit,2007.
    [11] FROLOV S M,AKSENOV V S,SHAMSHIN I O.Shock wave and detonation propagation through U-bend tubes[J].Proceedings of the Combustion Institute,2007,31(2):2421-2428.
    [12] FROLOV S M,AKSENOV V S,SHAMSHIN I O.Initiation of gaseous detonation in tubes with sharp U-bends[J].Doklady Physical Chemistry,2008,418(5):642-646.
    [13] FROLOV S M,AKSENOV V S,SHAMSHIN I O.Reactive shock and detonation propagation in U-bend tubes[J].Journal of Prevention in the Process Industries,2007,20(4/5/6):501-508.
    [14] FROLOV S M,AKSENOV V S,SHAMSHIN I O.Propagation of shock and detonation waves in channels with U-shaped bends of limiting curvature[J].Combustion and Explosion,2008,2(5):759-774.
    [15] SHINOBU O,MASAYA S,MAKOTO Y.Numerical Investigation on detonation wave through U-bend[J].Journal of Thermal Science,2010,19(6):540-544.
    [16] QIU Hua,SU Zheng,XIONG Cha.Experimental investigation on multi-cycle two-phase spiral pulse detonation tube of two configurations[J].Journal of Aerospace Engineering,2018,233(11):1-10.
    [17] 谭汶昊,郑龙席,黄康,等.U型脉冲爆震燃烧室的点火起爆工作特性试验研究[EB/OL].[2021-04-08].https:∥doi.org/10.13675/j.cnki.tjjs.200742
    [18] BROPHY C M,NETZER D W,SINIBALDI J,et al.Operation of a JP10/air pulse detonation engine[R].Huntsville,Alabama,US:the 36th AlAA/ASME/SAE/ASEE Joint Propulsion Conference,2000.
    [19] CICCARELLI G,GINSBERG T,BOCCIO J,et al.Detonation cell size measurements and predictions in hydrogen-air-steam mixtures at elevated temperatures[J].Combustion and Flame,1994,99(2):212-220.
    [20] CICCARELLI G.Flame acceleration in fuel-air mixtures at elevated initial temperatures[R].Indianapolis,Indiana,US:the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference,2002.
    [21] CARD J,CICCARELLI G.DDT in fuel-air mixtures at elevated temperatures and pressures[J].Shock Waves,2005,14(3):167-173.
    [22] WEN C S,CHUNG K M,LAI W H.Detonation initiation of JP-8-oxygen mixtures at different initial temperatures[J].Shock Waves,2012,22(5):477-482.
    [23] 李牧.多循环爆震起爆研究[D].西安:西北工业大学,2007.
    [24] STREHLOW R A.Gas phase detonations:recent developments[J].Combustion and Flame,1968,12(2):81-101.
    [25] ROY G D,FROLOV S M,BORISOV A A,et al.Pulse detonation propulsion:challenges,current status,and future perspective[J].Progress in Energy and Combustion Science,2004,30(6):549-552.
    [26] LU Jie,ZHENG Longxi,WANG Zhiwu,et al.Operating characteristics and propagation of back-pressure waves in a multi-tube two-phase valveless air-breathing pulse detonation combustor[J].Experimental Thermal and Science,2015,61:12-23.
    [27] IBRAHIM I A,FARAG T M,ABDEL-BAKY M E,et al.Experimental study of spray combustion characteristics of air-blast atomizer[J].Energy Reports,2020,6:209-215.
  • 加载中
计量
  • 文章访问数:  73
  • HTML浏览量:  7
  • PDF量:  58
  • 被引次数: 0
出版历程
  • 收稿日期:  2021-04-08
  • 刊出日期:  2022-03-28

目录

    /

    返回文章
    返回