期刊文献+

一种吸气式结构脉冲爆震发动机调节特性分析

Operating characteristics analysis for air-breathing pulse detonation engine
下载PDF
导出
摘要 介绍了一种吸气式脉冲爆震发动机的工作方式和推力计算方法。分析了脉冲爆震发动机的两种调节特性:变频特性和节流特性。分析表明,一定飞行状态下,当发动机可爆震混合物未充填满时,存在最佳的爆震频率,高于和低于此爆震频率都会降低脉冲爆震发动机的推进性能,此时必须采用节流的方式提高发动机推进性能。当存在多余隔离气体时,在改变爆震频率的同时增大平均供油量可以提高发动机的推进性能。因此实际调节脉冲爆震爆震发动机应尽量采用组合的调节方式。 The operation cycle and thrust calculation method for air-breathing pulse detonation engines are introduced. Two operating characteristics of pulse detonation engine are analyzed: regulation operating frequency characteristics and flow control characteristics. It is shown that an optimal operating frequency exists in a given flight regime when the detonation chamber is filled with partially detonable gas, The performance of the engine will decrease with lower or higher frequency. Thus fuel flow control method must be used to increase the performance of the engine. When there are redundant purge gases, the performance of the engine will increase with increasing operating frequency and fuel flow. Therefore, combined control method should be used for controlling pulse detonation engines.
出处 《推进技术》 EI CAS CSCD 北大核心 2006年第2期176-181,共6页 Journal of Propulsion Technology
基金 国家自然科学基金(50336030) 西北工业大学博士创新基金资助
关键词 脉冲爆震发动机 性能 调节特性^+ Pulse detonation engine Performance Control characteristics
  • 相关文献

参考文献7

  • 1Harris P G,Farinacio R,Stowe R A,et al.The effect of distance on impulse in a detonation tube[ R].AIAA 2001-3467.
  • 2Chiping Li,Kailasanath K.Performance analysis of pulse detonation engines with partial fuel filling[ R ].AIAA 2002-0610.
  • 3Wintenberger E,Austin J M,Cooper M,et al.An analytical model for the impulse of a single-cycle pulse detonation engine[ R].AIAA 2001-3811.
  • 4Wintenberger E,Shepherd J E.A model for the performance of air-breathing pulse detonation engines [ R ].AIAA 2003-4511.
  • 5Endo T,Yatsufusa T,Taki S,et al.Homogeneous-dilution model of partially-fueled pulse detonation engines [ R ].AIAA 2004-1214.
  • 6Takuma Endo,Jiro Kasahara,Akiko Matsuo et al.Pressure history at the thrust wall of a simplified pulse detonation engine [ J ].AIAA Journal,2004,42 (9).
  • 7樊思齐,徐芸华,等.航空推进系统控制[M].西安:西北工业大学出版社,2001.

共引文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部