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多管吸气式两相脉冲爆震发动机实验

张群 范玮

张群, 范玮. 多管吸气式两相脉冲爆震发动机实验[J]. 航空动力学报, 2012, 27(9): 1935-1938.
引用本文: 张群, 范玮. 多管吸气式两相脉冲爆震发动机实验[J]. 航空动力学报, 2012, 27(9): 1935-1938.
ZHANG Qun, FAN Wei. Experiment on multi-tube air-breathing two phase pulse detonation engine[J]. Journal of Aerospace Power, 2012, 27(9): 1935-1938.
Citation: ZHANG Qun, FAN Wei. Experiment on multi-tube air-breathing two phase pulse detonation engine[J]. Journal of Aerospace Power, 2012, 27(9): 1935-1938.

多管吸气式两相脉冲爆震发动机实验

基金项目: 国家自然科学基金(51176158); 西北工业大学基础研究基金(JC200912)

Experiment on multi-tube air-breathing two phase pulse detonation engine

  • 摘要: 研制了总长为1500mm,直径为200mm的6管并联吸气式两相脉冲爆震发动机实验器,在接近大气压条件下,以汽油为燃料、以空气为氧化剂成功进行了该发动机模型实验,实验中单爆震管最高工作频率达到35Hz,发动机整体最高工作频率达到210Hz.研究中发展了多管吸气式脉冲爆震发动机点火控 制策略,探索了不同点火控制策略对于发动机工作状态的影响规律,为将脉冲爆震发动 机用于工程实际提供了技术储备.

     

  • [1] Eidelmann S.Pulse detonation engine:a status review and technology development road map. AIAA 1997-2740,1997.
    [2] Falempin F,Bouchaud D,Forrat B.Pulsed detonation engine-possible application to low cost tactical missile and to space launcher. AIAA 2001-3815,2001.
    [3] Kailasanath K.Research on pulse detonation combustion systems:a status report. AIAA 2009-631,2009.
    [4] Roy G D,Frolov S M,Borisov A A,et al.Pulse detonation propulsion:challenges,current status,and future perspective[J].Progress Energy and Combustion Science,2004,30(6):545-672.
    [5] Matsuoka K,Esumi M,Ikeguchi K B,et al.Thrust measurement and visualization experiment of a multi-cycle single-tube pulse detonation. AIAA 2011-5789,2011.
    [6] Anderson E.Ball valve pulsed detonation engine. AIAA 2011-588,2011.
    [7] Piton D,Prigent A,Serre L,et al.Performance of a valveless airbreathing pulse detonation engine. AIAA 2004-3749,2004.
    [8] Frolov S M,Aksenov V S,Basevich V Y.Air-breathing liquid-fueled pulse detonation engine demonstrator[J].Doklady Physical Chemistry,2005,402(2):93-95.
    [9] 张群,严传俊,范玮,等.导弹用吸气式两相脉冲爆震发动机可行性研究[J].西北工业大学学报,2006,24(5):548-551. ZHANG Qun,YAN Chuanjun,FAN Wei,et al.Exploring feasibility of missiles employment of air-breathing two-phase PDE (pulse detonation engine)[J].Journal of Northwestern Polytechnical University,2006,24(5):548-551.(in Chinese)
    [10] Carter J,Lu F.Experiences in testing of a large-scale,liquid-fueled,air-breathing,pulse detonation engine. AIAA 2011-6089,2011.
    [11] Anderson S D,Tonouchi J H,Lidstone G L,et al.Performance trends for a product scale pulse detonation engine. AIAA 2004-3402,2004.
    [12] Chao T,Wintenberger E,Shepherd J E.On the design of pulse detonation engines. GALCIT Report FM00-7,2001.
    [13] 张群,严传俊,范玮,等.多循环脉冲爆震发动机概念化设计[J].推进技术,2003,24(6):500-504. ZHANG Qun,YAN Chuanjun,FAN Wei,et al.Conceptual design of multi-cycle pulse detonation engines[J].Journal of Propulsion Technology,2003,24(6):500-504.(in Chinese)
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出版历程
  • 收稿日期:  2011-11-10
  • 刊出日期:  2012-09-28

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