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.

[1]	Qiang XU, Hongliang CUI, Bangping DING, Aigang ZHAO, Yang ZHAO. Two-stage strong tracking differential Kalman filter for X-ray pulsar navigation with coloured noise [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(3): 526120-526120.
[2]	Bian LI, Lili QU, Yuping GAO. Methods for J0613-0200 steering a cesium clock [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(3): 526500-526500.
[3]	Guodong XU, Danlei ZHANG, Zhendong XU. Arrival time processing method of pulsar characteristic frequency signals [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(3): 526185-526185.
[4]	Yulin DING, Zhonghua HAN, Jianling QIAO, Han NIE, Wenping SONG, Bifeng SONG. Research progress in key technologies for conceptual-aerodynamic configuration design of supersonic transport aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626310-626310.
[5]	Yiran GU, Jiangtao HUANG, Shusheng CHEN, Deyuan LIU, Zhenghong GAO. Sonic boom inversion technology based on inverse augmented Burgers equation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626258-626258）.
[6]	Fangcheng SHI, Zhenxun GAO, Yuyan TIAN, Chongwen JIANG, Tiantian WANG, Chun-Hian LEE. Large eddy simulation of ideally expanded supersonic jet noise [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626266-626266.
[7]	Zhongchen LIU, Zhansen QIAN, Xuefei LI, Yan LENG, Dapeng GUO. Wind tunnel test techniques for exhaust nozzle plume effects on near-field sonic boom [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626952-626952.
[8]	Zeyong YIN, Yancheng YOU, Chengxiang ZHU, Jianfeng ZHU, Liaoni WU, Yue HUANG. Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 627181-627181.
[9]	Yong CHEN, Kelin ZHONG, Yue LUO, Miao WANG. Key technology and future development of regional airliner [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 26697-026697.
[10]	Fanmin MENG, Nuo MA, Wenchao MA, Junhui MENG, Wenguang LI. Wet modal analysis and tests for inflatable wing with swept air-beams [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 227098-227098.
[11]	Heng ZHANG, Jie LI, Binbin ZHAO. Improvement mechanism of ice-tolerance capacity for iced airfoil with variable camber of drooping leading edge [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627114-627114.
[12]	Xiong HUANG, Shiru QU, Heng ZHANG, Xiantiao CHEN. Stall performance of high-lift configuration of large civil aircraft with slat de-icing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627077-627077.
[13]	Jun SHU, Dongguang XU, Zhirong HAN, Si LI, Xiong HUANG. Hybrid wing design of icing wind tunnel supercooled large droplet icing test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627182-627182.
[14]	Yijian MA, Delin CHAI, Qiang WANG, Xian YI, Manzhao KONG. Phase change and adhesion characteristics of ice crystal movements in wing icing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627817-627817.
[15]	Feng ZHENG, Wei HUANG, Hongli JI, Jinhao QIU. Acoustic black hole effect of composite sheet structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 426453-426453.

Fan/Compressor Aero Design Technology for High Bypass Ratio Turbofan

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments