大涵道比涡扇发动机风扇/压气机气动设计技术分析

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2008, Vol. 29 ›› Issue (3): 513-526.

Fan/Compressor Aero Design Technology for High Bypass Ratio Turbofan

Chen Maozhang,Liu Baojie

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

Received:2008-03-21 Revised:2008-04-07 Online:2008-05-20 Published:2008-05-20
Contact: Liu Baojie

Abstract

Abstract:

Fan/compressor aero design technologies for the development of high bypass ratio turbofans are summarized, and their challenges on our development of high performance turbofan are analyzed. Some key technologies that need to be breakthrough are proposed.

Key words: large , commercial , airplane, , high , bypass , ratio, , fan, , compressor, , aero , design, , noise

CLC Number:

V231.3

Chen Maozhang;Liu Baojie. Fan/Compressor Aero Design Technology for High Bypass Ratio Turbofan[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 29(3): 513-526.

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Fan/Compressor Aero Design Technology for High Bypass Ratio Turbofan

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