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U型脉冲爆震燃烧室的点火起爆工作特性试验研究

Experimental Investigation on Ignition and Detonation Characteristics of U-Bend Pulse Detonation Combustor
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摘要 为缩短脉冲爆震燃烧室轴向长度,开展了气液两相U型脉冲爆震燃烧室(U-PDC)点火起爆特性试验研究。试验时采用火花塞点火和热射流点火,且点火能量可调。研究结果表明,两种点火方式均可实现U-PDC工作频率10~30Hz稳定工作,且爆燃向爆震转变DDT的时间随工作频率提高而缩短,为5~11ms。此外,实现U-PDC稳定工作时,热射流所需的点火能量为0.05J,较火花塞点火能量1J更低,并且热射流点火DDT距离更短,约718mm,起爆位置距来流入口的轴向距离约280mm,缩短了起爆所需的轴向长度,有利于工程应用。进一步提高热射流点火能量,其DDT距离无明显变化。 In order to shorten the axial length of pulse detonation combustor(PDC),experimental study on the ignition and detonation characteristics of a gas-liquid two-phase U-Bend pulse detonation combustor(UPDC)was carried out.Spark plug ignition and hot jet ignition were used in the experiment.The ignition energy is adjustable.The results indicate that the two ignition modes can achieve the stable operation of the U-PDC at the working frequency of 10~30Hz.The deflagration to detonation transition(DDT)time decreases with the increase of the working frequency,ranging from 5ms to 11ms.In addition,when the U-PDC works stably,the ignition energy required by hot jet is 0.05J,which is lower than that of spark plug ignition energy(i.e.1J).The DDT distance of hot jet ignition is shorter,about 718mm.The axial distance between detonation initiation position and the inlet is about 280mm,the shorter axial length required for detonation initiation is benefit for engineering application.However,the DDT distance sees no great variation when the ignition energy of hot jet further increases.
作者 谭汶昊 郑龙席 黄康 王凌羿 TAN Wen-hao;ZHENG Long-xi;HUANG Kang;WANG Ling-yi(School of Power and Energy,Northwestern Polytechnical University,Xi’an 710129,China;China Aerodynamics Research and Development Center,Mianyang 621000,China)
出处 《推进技术》 EI CAS CSCD 北大核心 2022年第1期167-174,共8页 Journal of Propulsion Technology
基金 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)。
关键词 脉冲爆震燃烧室 点火起爆特性 火花塞点火 热射流点火 点火能量 Pulse detonation combustor Ignition and initiation characteristics Spark plug ignition Hot jet ignition Ignition energy
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  • 1王治武,严传俊,范玮,熊姹,李牧.两相脉冲爆震发动机的燃油喷射、混合及其雾化研究[J].机械科学与技术,2005,24(11):1306-1309. 被引量:11
  • 2杨志,周凯元,谢立军,刘庚冉.Z型管道中气体火焰传播规律的实验研究[J].火灾科学,2006,15(3):111-115. 被引量:14
  • 3李牧,严传俊,王治武,邱华.无阀两相脉冲爆震发动机循环过程实验分析[J].推进技术,2007,28(1):97-102. 被引量:9
  • 4Fan W,Yan C J,Huang X Q,et al.Experimental investigation on two-phase pulse detonation engine[J].Combustion and Flame,2003,133 (4):441-450.
  • 5Cooper M,Jackson S,Shepherd J E.Effect of deflagration-detonation transition on pulse detonation engine impulse[R].GALCIT Report FM00-3.
  • 6Benedick W,Guirao C,Knystautas R,et al.Critical charge for the direct initiation of detonation in gaseous fuel/air mixtures[J].Prog.Astro.Aero.,1986,106(2):181-202.
  • 7Sinibaldi J O,Brophy C M,Robinson J P.Ignition effects on defiagration-to-detonation transition distance in gaseous mixtures[R].AIAA 2000-3590.
  • 8Santoro R J,Conrad C,Lee S Y,et al.Fundamental multi-cycle studies of the performance of pulse detonation engines[R].ISABE 2001-1171.
  • 9Brophy C M,Netzer D W,Forester D.Detonation studies of JP-10 with oxygen and air for pulse detonation engine development[R].AIAA 98-4003.
  • 10Brophy C M,Netzer D W,Sinibaldi J,et al.Detonation of a JP-IO aerosol for pulse detonation applications[A].High-speed deflagration and detonation:fundamentals and control[C].Moscow,2001.

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