| 脉冲爆震发动机倒旋流气动阀性能实验 |
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| 引用本文： | 宫继双,范育新,张义宁,齐海帆,程晓军,王家骅,张靖周.脉冲爆震发动机倒旋流气动阀性能实验[J].推进技术,2012,33(4):657-664. |
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| 作者姓名： | 宫继双 范育新 张义宁 齐海帆 程晓军 王家骅 张靖周 |
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| 作者单位： | 1. 南京航空航天大学能源与动力学院,江苏南京,210016
2. 中国航天科工集团三十一研究所,北京,100074 |
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| 基金项目： | 高超声速冲压发动机技术重点实验室项目资助 |
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| 摘 要： | 为了得到高性能的脉冲爆震发动机气动阀,根据以前研究者气动阀设计的经验,提出倒旋流气动阀设计思想,以此设计思想设计了五种结构不同的气动阀,并分别对五种气动阀性能进行了冷态和热态试验研究。试验结果表明:倒旋流数越大气动阀的单向性能越好;在进气道进口加装长1.5D(D为进气道进口直径)的直管,可获得最佳的气动阀单向性;综合考虑进气总压损失和气动阀单向性等因素,认为轴向倒旋流气动阀更适合PDE应用。通过轴向气动阀的热态试验结果表明:采用倒旋流设计的气动阀,可有效抑制前传压力约70%。
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| 关 键 词： | 脉冲爆震发动机 气动阀 倒旋流 单向性能 堵塞比 |
Experimental Investigation on Inversing-Rotating Aero-Valve in PDE |
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| GONG Ji-shuang,FAN Yun-xin,ZHANG Yi-ning,QI Hai-fan,CHENG Xiao-jun,WANG Jia-hua,ZHANG Jing-zhou.Experimental Investigation on Inversing-Rotating Aero-Valve in PDE[J].Journal of Propulsion Technology,2012,33(4):657-664. |
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| Authors: | GONG Ji-shuang FAN Yun-xin ZHANG Yi-ning QI Hai-fan CHENG Xiao-jun WANG Jia-hua ZHANG Jing-zhou |
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| Institution: | 1(1.College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China; 2.The 31st Research Institute of CASIC,Beijing 100074,China) |
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| Abstract: | In order to obtain high performance aero-valve of Pulse Detonation Engine(PDE),a new type of aero-valve,called inversing-rotating aero-valve,was advanced by summarizing the experience of former designers.Five aero-valves with different structures were designed for following experiment.Results show that aero-valves with larger swirl number SN,which are fixed straight tubes(1.5D long) ahead of inlet,have more attractive one-way performance.The axial inversing-rotating aero-valve shows up more adaptability for PDE,while considering pressure loss and one-way performance.Furthermore,the pressure of travelling waves to upstream through valve can be decreased about 70%. |
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| Keywords: | Pulse detonation engine Aero-valve Inversing-rotating One-way performance Block ratio |
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