民用大涵道比涡扇发动机叶轮机某些关键技术

邹正平; 李宇; 刘火星; 张正秋; 叶建; 李维; 陈竞炜

民用大涵道比涡扇发动机叶轮机某些关键技术

1.
北京航空航天大学能源与动力工程学院航空发动机气动热力重点实验室航空发动机数值仿真研究中心, 北京 100191
2.
中国航空动力机械研究所, 株洲 412002

基金项目: 国家自然科学基金(50776003);北京航空航天大学蓝天新星计划项目

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- 被引次数: 0
出版历程
- 收稿日期: 2007-08-09
- 修回日期: 2007-11-07
- 刊出日期: 2008-08-28

Key turbomachinery technology of civil high-bypass-ratio turbofan engine

1.
School of Jet Propulsion, National Key Laboratory on Aero-Engines, Aeroengine Numerical Simulation Research Center, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2.
Chinese Aviation Powerplant Research Institute, Zhuzhou 412002, China

摘要

摘要: 结合国内外的相关研究工作,对大涵道比涡扇发动机叶轮机部分设计技术研究进展进行了总结和分析,从风扇/压气机设计技术、涡轮设计技术、流动及噪声控制和多学科耦合四个方面阐述了我国发展大涵道比发动机需要解决的部分叶轮机关键技术.
- 叶轮机关键技术 /
- 民用发动机 /
- 大涵道比 /
- 涡扇发动机 /
- 叶轮机
Abstract: The research progress on partial turbomachinery technology of high-bypass-ratio turbofan engine were reviewed and analyzed in the present study and the partial key technology of turbomachinery required for our country's high-bypass-ratio turbofan engine were also expatiated.The main contents included four aspects: fan/compressor design technique,turbine design technique,flow and noise control and multi-disciplinary coupling technique.
- key turbomachinery technology /
- civil engine /
- high-bypass-ratio /
- turbofan /
- turbomachinery

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