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脉冲爆震燃烧效率的探索性试验研究
引用本文:黄希桥,严传俊,范玮,邱华,王治武.脉冲爆震燃烧效率的探索性试验研究[J].航空动力学报,2006,21(6):962-966.
作者姓名:黄希桥  严传俊  范玮  邱华  王治武
作者单位:西北工业大学,动力与能源学院,西安,710072
摘    要:为了对脉冲爆震燃烧过程的燃烧效率有一个初步了解,在分析脉冲爆震发动机工作原理的基础上,设计了一套带有压力可调单向阀结构的取样系统,并进行了试验验证.试验针对爆震频率为5Hz、当量比为1的汽油和空气混气,测试了爆震波充分发展前后不同位置处爆震燃烧过程的燃烧效率,结果表明可以利用设计的取样系统进行脉冲爆震发动机燃烧效率的测量,试验还发现在脉冲爆震室后爆震发展比较充分的位置,测取的燃烧效率比较高,最高可达99.6%.

关 键 词:航空、航天推进系统  脉冲爆震发动机  取样系统  燃烧效率  试验研究
文章编号:1000-8055(2006)06-0962-05
收稿时间:1/5/2006 12:00:00 AM
修稿时间:2006年1月5日

Preliminary experimental study of pulse detonation combustion efficiency
HUANG Xi-qiao,YAN Chuan-jun,FAN Wei,QIU Hua and WANG Zhi-wu.Preliminary experimental study of pulse detonation combustion efficiency[J].Journal of Aerospace Power,2006,21(6):962-966.
Authors:HUANG Xi-qiao  YAN Chuan-jun  FAN Wei  QIU Hua and WANG Zhi-wu
Institution:School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:A sampling system with a variable pressure check valve was designed to investigate the combustion efficiency of pulse detonation combustion process on the basis of the pulse detonation engine(PDE) operating principle analysis.With the designed sampling system,the combustion efficiencies of the pulse detonation combustion processes using gasoline as fuel and compressed air as oxidizers at operating frequency of 5 Hz were measured both at conditions that the steady and fully developed detonation waves were formed and not formed.The experimental results indicate that the pulse detonation combustion efficiency can be measured successfully using the designed sampling system.The combustion efficiency where the detonation waves have fully developed is higher than that of not fully developed. The highest combustion efficiency is up to 99.6%.
Keywords:aerospace propulsion system  Pulse Detonation Engine(PDE)  sampling system  combustion efficiency  experimental study
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