Design and experiment demonstration of a booster of small turbofan engine

DING Jian-guo; ZOU Xue-qi; Wu Zhi-qing; YANG Jing-jing; HU Jun

Chinese

您当前的位置：

首页 >

文章列表页 >

Design and experiment demonstration of a booster of small turbofan engine

更新时间：2026-07-07

- Design and experiment demonstration of a booster of small turbofan engine
- Vol. 23, Issue 8, (2008)
- 作者机构：
  
  1. 南京航空航天大学能源与动力学院,南京,210016
  2. 中国航空动力机械研究所,株洲,412002
  3. 北京航空航天大学能源与动力工程学院,北京,100191
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2008
- 稿件说明：
移动端阅览
DING Jian-guo, ZOU Xue-qi, Wu Zhi-qing, et al. Design and experiment demonstration of a booster of small turbofan engine[J]. 2008, 23(8).
DOI：

DING Jian-guo, ZOU Xue-qi, Wu Zhi-qing, et al. Design and experiment demonstration of a booster of small turbofan engine[J]. 2008, 23(8). DOI：

摘要

采用经过试验验证的一维方案设计程序包以及与轴对称流设计程序相匹配的任意中弧线叶片造型程序

运用三维计算与一维、二维气动设计相结合的方法成功地完成了某小涡扇发动机增压级气动设计

并且单独设计和加工内涵两级增压级进行了试验验证

试验结果表明

该增压级具有宽广的高效率区和高喘振裕度

设计结果与试验结果吻合较好.

Abstract

By means of test-proven one dimension project design procedure library and arbitrary airfoils blade design procedure of turbo machine matching the axial symmetry streamline curvature approach design code

a booster of small turbofan engine was designed and tested successfully by combining three dimension computational fluid dynamics

one dimension and two dimension aero-dynamics designs.The experiment results indicate that

the booster has high efficiency over a wider range and better stall margin

and the design results correspond with experimental results.

关键词

Keywords

references

Views

501

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Design and numerical investigation of RBCC prototype inlet

A design method of mixed flow fan for helicopters

Study on turbine aerodynamics design of small turbofan engines

Design of rotor system for micro turbine jet engine

Design and core and bypass numerical simulation of acompound swept fan

Related Author

LIU Xiao-wei

LIU Pei-jin

QIN Fei

HE Guo-qiang

SHI Lei

CHANG Li

YU Jian-zu

GAO Hong-xia

Related Institution

Science and Technology on Combustion,Internal Flow and Thermal-structure Laboratory, College of Astronautics, Northwestern Polytechnical University

Chinese Helicopter Research and Development Institute, Aviation Industry Corporation of China

School of Aeronautical Science and Engineering, Beijing University of Aeronautics and Astronautics

China Aviation Powerplant Research Institute, Aviation Industry Corporation of China

National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰