Volume 28 Issue 10
Oct.  2013
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CHENG Xiao-jun, FAN Yu-xin, CAI Di, HAN Qi-xiang, WANG Jia-hua. Comparative ignition characteristics of ethylene and gasolene in multi-cycle pulse detonation engine[J]. Journal of Aerospace Power, 2013, 28(10): 2276-2283.
Citation: CHENG Xiao-jun, FAN Yu-xin, CAI Di, HAN Qi-xiang, WANG Jia-hua. Comparative ignition characteristics of ethylene and gasolene in multi-cycle pulse detonation engine[J]. Journal of Aerospace Power, 2013, 28(10): 2276-2283.

Comparative ignition characteristics of ethylene and gasolene in multi-cycle pulse detonation engine

  • Received Date: 2012-09-26
  • Publish Date: 2013-10-28
  • To investigate the influence of the structure of multi-cycle pulse detonation engine(PDE) on its operation performance,experiments of ethylene-air and gasoline-air mixtures initiation process in the aero-valve PDE of 1050mm length and 40mm inner diameter were performed.The results show that the detonation wave can be successfully initiated in the ethylene-air with frequency of 25,30Hz and 40Hz,and C-J(Chapman-Jouguet) detonation wave can be achieved at the frequency of 40Hz with detonation wave propagation velocity of 1724m/s(less 5.6% than the C-J detonation wave velocity theoretical value 1832.45m/s) and peak wave pressure of 3.01MPa(higher 7.88% than the C-J detonation wave pressure theoretical value 2.79MPa).While the deflagration to detonation transition failed to complete in gasolene-air.By comparison of the two results,it was found that the evaporation process dominated the initiation process in liquid fuels,thus slowering the flame acceleration process in the detonation tube.More novel and optimized-designed reinforced-combustion devices for accelerating the flame should be developed,which may cause higher total pressure loss.Thus,atomization and evaporation to improve the quality of the mixture is a key technology for detonation in the liquid fuel.

     

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  • [1]
    Brophy C M,Sinibaldi J O,Netzer,et al.Operation of a JP-10/air pulse detonation engine [R].AIAA 2000-3591,2000.
    [2]
    Brophy C M,Netzer D W,Dorester D.Detonation studies of JP10/air with oxygen and air for pulse detonation engine development [R].AIAA 98-4003,1998.
    [3]
    Brophy C M,Sinibaldi J O,Damphousse P.Initiator performance for liquid-fueled pulse detonation engine [R].AIAA 2002-0472,2002.
    [4]
    范育新.大管径气动阀式两相脉冲爆震发动机几个关键技术研究[D].南京:南京航空航天大学,2005. FAN Yuxin.Investigation on several key technologies of two-phase valveless large-scale pulse detonation engine [D].Nanjing:Nanjing University of Aeronautics and Astronautics,2005.(in Chinese)
    [5]
    张义宁,王家骅,张靖周.频率30~50Hz两相脉冲爆震发动机研究[J].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.(in Chinese)
    [6]
    张义宁.提高两相脉冲爆震发动机工作频率的研究[D].南京:南京航空航天大学,2007. ZHANG Yining.Investigation on increasing operating frequency of two-phase pulse detonation engine [D].Nanjing:Nanjing University of Aeronautics and Astronautics,2007.(in Chinese)
    [7]
    宫继双,范育新,王家骅.两相多循环扇形PDE试验研究[J].航空动力学报,2008,23(11):2068-2074. GONG Jishuang,FAN Yuxin,WANG Jiahua.Experimental investigation on two-phase and mutli-cycle sector-PDE [J].Journal of Aerospace Power,2008,23(11):2068-2074. (in Chinese)
    [8]
    Danaher T J.Characterization of ethylene/JP-10 fuel injection profiles for a valveless pulse detonation Engine [D].California,US:Naval Postgraduate School,2007.
    [9]
    Sexton N G.Detonability of hydrocarbon-air mixtures using combustion enhancing geometries for pulse detonation engines [D].California,US:Naval Postgraduate School,2001.
    [10]
    Hackard Jr C N.Ignition characteristics for transient plasma ignition of ethylene-air and JP-10-Air mixtures in a pulse detonation engine [D].California,US:Naval Postgraduate School,2007.
    [11]
    LI Chiping,Kailasanath K.Detonation initiation in pulse detonation engines [R].AIAA 2003-1170,2003.
    [12]
    Hutcheson P,Brophy C,Sinibaldi J.Investigation of flow field properties on detonation initiation [R].AIAA 2006-5099,2006.
    [13]
    Shimo M,Heister S.Multicyclic detonation initiation studies in valveless pulsed detonation combustors [R].AIAA 2006-4308,2006.
    [14]
    Roya G D,Frolovb 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):545-672.
    [15]
    严传俊,范玮.脉冲爆震发动机原理及关键技术[M].西北工业大学出版社,2006.
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