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Volume 28 Issue 5
May  2002
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Journal of Beijing University of Aeronautics and Astronautics  > 2002  >  28(5): 490-496.
LIU Da-xiang, CHENG Rong-hui. Current Status and Development Direction of Aircraft Power Technology in the World[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(5): 490-496. (in Chinese)
Citation: LIU Da-xiang, CHENG Rong-hui. Current Status and Development Direction of Aircraft Power Technology in the World[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(5): 490-496. (in Chinese)
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Current Status and Development Direction of Aircraft Power Technology in the World

  • 1.

    Beijing University of Aeronautics and Astronautics, Dept. of Propulsion

  • 2. China Gas Turbine Establishment

  • Received Date: 01 Feb 2002
  • Publish Date: 31 May 2002
    Abstract
  • The development course of jet engine is described. The engine which thrust weight ratio is about 8 is the power of the main fighters on active service in the developed countries. The 4th generation fighters stalling the jet engine with thrust weight ratio 10 will be gradually equipped with the army after 2003~2007, and will become the main fighting aircraft of USA and some western countries and even several neighbor countries and area of China after 2010. This paper sums up the development and key technologies of civil turbo\|fan engine and power of helicopter. The aero\|engine development will be confronted with new opportunities in the 21st century. The development direction of the main key technologies on the aircraft power in the 21st century is indicated.

     

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    • References(1)
  • [1] 方昌德.军用涡喷/涡扇发动机和通用推进技术 .见:迈向21世纪的航空科学技术 .北京:航空工业出版社,1994. [2]王定勇.民用涡扇发动机技术 .见:迈向21世纪的航空科学技术 .北京:航空工业出版社,1994. [3]艾 青.涡桨/涡轴发动机技术 .见:迈向21世纪的航空科学技术 .北京:航空工业出版社,1994. [4]Koop W. The integrated high performance turbine engine technology program ． ISABE 977175, 1997.
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