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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2015, Vol. 36 ›› Issue (8): 2563-2576.doi: 10.7527/S1000-6893.2015.0078

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

Some problems and thoughts in the development of aero-engine fan/compressor

LIU Yongquan1, LIU Taiqiu1, JI Luchen2   

  1. 1. AVIC Shenyang Engine Design and Research Institute, Shenyang 110015, China;
    2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
  • Received:2015-05-04 Revised:2015-06-19 Online:2015-08-15 Published:2015-06-19
  • Contact: 10.7527/S1000-6893.2015.0078 E-mail:yqliu606@vip.sina.com

Abstract:

In the next 10 to 20 years, China's aero-engine technology will usher in a golden opportunity for development, which we must be fully prepared for. This paper focuses on the aerodynamic field of the aero-engine core components-fan/compressor. Firstly, from the point of design methods, theories and the still existing questions of aerodynamics, we sort out the international development trend. Then against the fundamental research and innovation, etc., we describe the civil development status and problems; finally we analyze the future development, thoughts and emphasis of fan/compressor, which is expected to offer some reference for the research of China's military and civil aero-engine fan/compressor.

Key words: aero-engine, fan, compressor, technology research, technology system, developing trend

CLC Number: