推进技术 ›› 2001, Vol. 22 ›› Issue (2): 89-91.

• •    下一篇

军用航空发动机加力控制系统的研究和发展

朴英,张绍基   

  1. 北京航空航天大学动力系!北京100083;沈阳航空发动机研究所!辽宁沈阳100015
  • 发布日期:2021-08-15

Research and development of afterburner control system for military aeroengine

  1. Dept.of Jet Propulsion,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;Shenyang Aeroengine Research Inst.,Shenyang 110015,China
  • Published:2021-08-15

摘要: 对国外军用航空发动机加力控制系统的研制现状和今后的发展方向进行了归纳和分析 ,讨论了加力燃油泵、加力燃油调节器、加力燃油计量和分配装置、喷口油源泵和喷口调节器的技术特点、方案选择和研究动向。全权限数字电子控制技术的研究和应用 ,将会对军用航空发动机的研究和发展产生巨大的影响。

关键词: 航空发动机;加力燃烧室;燃料系统;发动机控制;控制系统;述评

Abstract: The performance of the afterburner control system for the advanced military aeroengine is very important.It’s afterburner and control system have been for many years.With the development of the FADEC and the application of the new composite,the afterburner control system tends to be electrical,small scale and integrative direction,which will significantly improve the performance of the military aeroengine.

Key words: Aircraft engine;Afterburner;Fuel system;Engine control;Control system;Review