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气动阀式脉冲爆震发动机部分充填机理研究
引用本文:李建中,王家骅,范育新,张义宁,张靖周.气动阀式脉冲爆震发动机部分充填机理研究[J].航空动力学报,2006,21(1):45-49.
作者姓名:李建中  王家骅  范育新  张义宁  张靖周
作者单位:南京航空航天大学,能源与动力学院,北京,210016
摘    要:研究了不同部分充填比例对煤油/空气气动阀式脉冲爆震发动机(PDE)的爆震波压力特性影响,初步分析了部分充填的爆震管内一系列波相互作用的机理.研究结果表明,在气动阀选定、爆震管长度和爆震管内部结构一定条件下,随着脉冲爆震发动机可爆混气充填爆震管比例的降低,虽然爆震波压力峰值略有下降,但是,单位体积可爆混气获得的冲量线性增加,提高了脉冲爆震发动机的工作性能.研究结果对于煤油/空气气动阀式脉冲爆震发动机的总体优化设计,提高PDE的工作性能具有重要的参考价值.

关 键 词:航空、航天推进系统  脉冲爆震发动机  爆震燃烧  气动阀  部分充填
文章编号:1000-8055(2006)01-0045-05
收稿时间:2004/11/2 0:00:00
修稿时间:2004年11月2日

Investigation on Pneumatic-Valve Pulse Detonation Engine with Partial Detonable Mixture Filling
LI Jian-zhong,WANG Jiahu,FAN Yu-xin,ZHANG Yi-ning and ZHANG Jing-zhou.Investigation on Pneumatic-Valve Pulse Detonation Engine with Partial Detonable Mixture Filling[J].Journal of Aerospace Power,2006,21(1):45-49.
Authors:LI Jian-zhong  WANG Jiahu  FAN Yu-xin  ZHANG Yi-ning and ZHANG Jing-zhou
Institution:1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;1.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Effects of partial detonable mixture filling proportion on detonation wave pressure properties of kerosene/air pneumatic-valve pulse detonation engine were investigated.A preliminary analysis of a series of wave's reciprocity was carried out.Experimental results show that with given double swirl and direct pneumaticvalve and detonation tube structure,the decrease of partial detonable mixture filling proportion causes a little decrease of the peak value of detonation waves' pressure,but impulse per unit volume of detonable mixture increases linearly.This investigation is important to the design optimization of the kerosene/air pneumatic-valve PDE,and to improve the performance of PDE.
Keywords:aerospace propulsion system  pulse detonation engine  detonative combustion  pneumatic-valve  partial filling
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