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无人机和巡航导弹用涡扇/涡喷发动机的设计特点 被引量:9

Design Characteristics of Turbofan/Turbojet engines for UAV/Cruise Missile Application
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摘要 无人机和巡航导弹发动机有许多共性,人们有时候会把它们混淆。本文详细分析了无人机和巡航导弹的区别,对比研究了它们对发动机的要求和关键属性,随后分析了无人机和巡航导弹对涡扇/涡喷发动机的特殊要求与设计特性,以及目前正在开发的先进技术。 Cruise missiles are occasionally confused with UAVs because they are both unmanned. Their distinctions are clearly made in this paper. The requirements and key attributes of engines for UAW cruise missile applications are introduced. The special requirements and design characteristics are subsequently analyzed, and the advenced technologies under development currently are also described.
作者 郭琦 李兆庆
出处 《燃气涡轮试验与研究》 2007年第2期58-62,共5页 Gas Turbine Experiment and Research
关键词 涡扇发动机 设计特点 无人飞行器 巡航导弹 turbofan engines design characteristics UAVs cruise missiles
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参考文献6

  • 1Office of the Secretary of Defense. Unmanned Aircraft Systems Roadmap[R]. 2005-2030.
  • 2田宁.小推力涡扇发动机的先进制造技术[J].航空制造技术,2005,48(3):53-55. 被引量:1
  • 3Richard N J, Development of Engines for Unmanned Air Vehicles: Some Factors To Be Considered [R]. ADA412680,2003.
  • 4Bradbrook S J. Common Solutions to Commercial and Military Propulsion Requirements [C]//24th International Congress of the Aeronautical Sciences, 2004.
  • 5Ehrlich H,Kurz K H,Rued K P,et al. Trends in Military Aeroengine-Design-from EJ200 to Future Manned and Unmanned Vehicle Propulsion [R]. AIAA 2003-2612, 2003.
  • 6Cruise Missile Technologies and Performance Analysis[J/ OL]. Jane's Strategic Weapon Systems,(2005-11-10). http://www.jane's.com.

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