Volume 22 Issue 2
Feb.  2007
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ZHANG Yi-Ning, WANG Jia-Hua, LIU Hong, ZHANG Jing-zhou. Investigation of several delay times in operation process of multi-cycle pulse detonation engine[J]. Journal of Aerospace Power, 2007, 22(2): 228-232.
Citation: ZHANG Yi-Ning, WANG Jia-Hua, LIU Hong, ZHANG Jing-zhou. Investigation of several delay times in operation process of multi-cycle pulse detonation engine[J]. Journal of Aerospace Power, 2007, 22(2): 228-232.

Investigation of several delay times in operation process of multi-cycle pulse detonation engine

  • Received Date: 2006-01-04
  • Rev Recd Date: 2006-03-27
  • Publish Date: 2007-02-28
  • In order to promote the operating coordination of a two-phase pulse detonation engine(PDE),the delay time of detonation and operating performance of the solenoid valve were experimentally studied by using ion-sensors and pressure transducers of high-frequency response.The detonation tube is of 58mm inner diameter and 1 270 mm long.Liquid gasoline/air mixture is filled for the engine multi-cycle operations.According to the research,the mixture ignition delay is 3~4.5 ms,the aero-valve closing delay is 4.9~6.4 ms,and the solenoid electric valve on/off delay time is 2.4 ms and 3.4 ms respectively.The transition time from deflagration-to-detonation is about 3.0~3.8 ms.The solenoid electric valve cannot operate orderly when the engine operating frequency is higher than 20 Hz.These data obtained are helpful to coordinate PDE operation process.

     

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  • [1]
    Goracke D B,Levack D J H.Tripropellant engine drive cycle considerations for the SSTO application[R].AIAA95-2950.
    [2]
    Manski D,Goertz C,Sassnick H,et al.Cycles for earth-to-orbit propulsion[J].Journal of Propulsion and Power.1998,14(5):588-604.
    [3]
    Colasurdo G,Pastrone D,Casalino L.Optimal performance of a dual-fuelsingle-stage rocket[J].Journal of Spacecraft and Rockets,1998,35(5):667-671.
    [4]
    Chao T W,Wintenberger E,Shepherd J E.On the design of pulse detonation engines[R].GALCIT Report FM00-7,2001.
    [5]
    Bussing T R A,Bratkovich T E,Hinkey Jr J B.Practical implementation ofpulse detonation engines[R].AIAA 97-2748.
    [6]
    Kentfield J A C.The potential of valveless pulsejets for small UAV propulsion applications[R].AIAA 98-3879
    [7]
    Cooper M,Jackson S,shepherd J E.Effect of deflagration-detonation transition on pulse detonation engine impulse[R].CALCIT Report FM00-3,2000.
    [8]
    范育新,王家骅,李建中,等.脉冲爆震发动机工作过程控制和协调试验[J].推进技术,2004,25(6):538-542.FAN Yuxin,WANG Jiahua,LI Jianzhong,et al.Experimental investigation on working process of pulse detonation engine (PDE)[J].Journal of Propulsion Technology,2004,25(6):538-542.
    [9]
    张义宁,王家骅,张靖周.频率30~50Hz两相脉冲爆震发动机研究.航空学报2006,27(6):993-997.ZHANG Yining,WANG Jiahua,ZHANG Jingzhou,Investigation on two phase pulse detonation engine at the frequency 30~50Hz[J].Acta Aeronautica et Astronautica Sinica,2006,27(6):993-997.
    [10]
    范育新,王家骅,李建中,等.脉冲爆震发动机供油自适应控制优化设计研究[J].推进技术,2005,26(1):62-67.FAN Yuxin,WANG Jiahua,LI Jianzhong,et al.Mechan-ism of fuel self-fit control in pulse detonation engine[J].Journal of Propulsion Technology,2005,26(1):62-67.
    [11]
    张义宁,王家骅,张靖周.两相多循环爆震波特性研究[J].航空动力学报,2006,21(5):789-794.ZHANG Yining,WANG Jiahua,ZHANG Jingzhou.Investigation on two-phase and multi-cycle detonation[J].Journal of Aerospace Power,2006,21(5):789-794.
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