径向进气多管脉冲爆震发动机设计

推进技术 ›› 2011, Vol. 32 ›› Issue (5): 746-750.

• • 上一篇

径向进气多管脉冲爆震发动机设计

张义宁,刘振德,王云雷,陈宝延

中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室;中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室;中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室;中国航天科工集团三十一研究所高超声速冲压发动机技术重点实验室

发布日期:2021-08-15

Design of multi-detonator pulse detonation engine with fuel/air mixture radial filling

Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China;Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China;Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China;Science and Technology on Scramjet Lab.,The 31st Research Inst.of CASIC,Beijing 100074,China

Published:2021-08-15

摘要/Abstract

摘要： 为了缩短脉冲爆震发动机工作过程中混气充填时间,采用旋转筒控制爆震室径向进气,设计了结构更为合理的多爆震室PDE试验原型机。该原型机可以在较短时间内完成爆震室的混气充填,为热态爆震燃烧过程留出更充裕的时间,对提高PDE工作频率和整机性能有促进作用。

关键词: 爆震;脉冲爆震发动机;旋转阀;设计

Abstract: In order to shorten the time of fuel and air mixture(FAM)filling in pulse detonation engine(PDE) operation process,a multi-detonator PDE with reasonable construction is designed,and it has shown good performance.The FAM filling is along the radial direction and governed by a rotary-tube.This characteristic makes the FAM filling process finished in a short time and saves time for detonation process,and it is helpful for improving the prototype operation frequency and efficiency.

Key words: Detonation;Pulse detonation engine(PDE);Rotary valve;Design

张义宁,刘振德,王云雷,陈宝延. 径向进气多管脉冲爆震发动机设计[J]. 推进技术, 2011, 32(5): 746-750.

径向进气多管脉冲爆震发动机设计

Design of multi-detonator pulse detonation engine with fuel/air mixture radial filling

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