Modeling of whole processes of mixing exhaust afterburner twin spool turbofan engine

SHI Rui-jun; ZHOU Jian-bo; ZHANG Qiu-gui; PI Xing; FAN Si-qi

Chinese

您当前的位置：

首页 >

文章列表页 >

Modeling of whole processes of mixing exhaust afterburner twin spool turbofan engine

更新时间：2026-07-07

- Modeling of whole processes of mixing exhaust afterburner twin spool turbofan engine
- Vol. 28, Issue 10, (2013)
- 作者机构：
  
  1. 中国航空工业集团公司中国航空动力机械研究所,湖南,株洲,412002
  2. 西北工业大学动力与能源学院,西安,710072
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2013
- 稿件说明：
移动端阅览
SHI Rui-jun, ZHOU Jian-bo, ZHANG Qiu-gui, et al. Modeling of whole processes of mixing exhaust afterburner twin spool turbofan engine[J]. 2013, 28(10).
DOI：

SHI Rui-jun, ZHOU Jian-bo, ZHANG Qiu-gui, et al. Modeling of whole processes of mixing exhaust afterburner twin spool turbofan engine[J]. 2013, 28(10). DOI：

摘要

根据部件法建立了加力式双转子混合排气涡扇发动机全包线稳态数学模型.基于该模型

利用容积动力学原理

建立了起动数学模型.将该原理扩展到慢车状态以上

建立了包括起动、加减速、开关加力、停车等完整过程的全状态动态数学模型.以此为基础

给出了加力式双转子混合排气涡扇发动机在飞行包线内的高度特性.根据加力式双转子混合排气涡扇发动机原理

设计了简单的起动调节规律、加减速调节规律、加力调节规律及停车调节规律;计算了海平面标准大气条件下的从起动、加减速、开关加力、停车的完整动态过程.理论分析与仿真结果表明:该建模方法能够正确完成加力式双转子混合排气涡扇发动机的全包线的稳态计算和全状态动态计算

准确反映了该发动机在整个飞行包线内的全部工作过程.

Abstract

Firstly

a steady state mathematical model was developed for the mixing exhaust afterburner twin spool turbofan engine in full envelope. Secondly

a startup dynamic model was constructed by combining the effects of volume dynamics with the steady model. Then

by extending the volume dynamics theory to idle state

a whole process model was obtained to calculate the startup process

acceleration and deceleration process

turn on/off afterburner process and stop process. Finally

the altitude characteristic was presented with the proposed regulation law in full envelope of the engine; the whole processes from startup to stop were simulated with the designed control algorithm. The results show that the model is able to simulate the steady and dynamic states in full envelope

and correctly describes the whole process of mixing exhaust after burner twin spool turbofan engine including afterburning.

关键词

Keywords

references

Views

1327

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Numerical study and verification on combustion characteristics of afterburner with chevron mixer

Numerical study on the combustion characteristics of afterburner with chevron mixer

Analysis of components infrared radiation of afterburning turbofan engine under non-afterburning condition

Superiority analysis of CCA technology under typical flight mission

Infrared radiation signature of three bearing swivel nozzle

Related Author

DI Hu-wei

SHAN Yong

GAO Jia-chun

ZHANG Jing-zhou

LIU Tao

WANG Ya-meng

XU Xing-ping

HUANG Wei

Related Institution

College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics

Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China

Department of Aerial Four Stations,Xuzhou Air Force College, The Chinese Peoples Liberation Army

School of Energy and Power Engineering，Beihang University

National Key Laboratory of Science and Technology on Aero⁃Engine Aero⁃thermodynamics，Beihang University

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