Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations

HUANG Kai-ming; YIN Ze-yong; HUANG Jing-quan

Chinese

您当前的位置：

首页 >

文章列表页 >

Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations

更新时间：2026-07-07

- Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations
- Vol. 21, Issue 2, (2006)
- 作者机构：
  
  1. 南京航空航天大学能源与动力学院,江苏,南京,210016
  2. 中国航空动力机械研究所,湖南,株洲,412002
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2006
- 稿件说明：
移动端阅览
HUANG Kai-ming, YIN Ze-yong, HUANG Jing-quan. Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations[J]. 2006, 21(2).
DOI：

HUANG Kai-ming, YIN Ze-yong, HUANG Jing-quan. Analysis of Turbo-Shaft Engine Control System Dynamic Performance with Parameter Limitations[J]. 2006, 21(2). DOI：

摘要

通过研究涡轴发动机的限制参数

提出了涡轴发动机控制系统中可能采用的限制规律并建立了一个带多种限制模块的数字控制器

以某型涡轴发动机数学模型为控制对象

对带限制参数和不加限制的过渡态控制进行了仿真对比

给出了地面和空中的仿真结果

结果表明不同的限制参数组合会对发动机的过渡态性能产生不同的影响

在控制系统中合理选取限制参数及限制值能够优化发动机过渡态性能。

Abstract

Effect of limitations of aero-engine parameters was studied.The purpose of the analysis was to achieve better dynamic performance.Limitation rules that may be adopted in turbo-shaft engine control system were presented and a digital controller with multiple limitation loops was designed.Simulation results show that different limitations of parameters bring different effects on engine dynamic performance.Selecting limitations of parameters reasonably can optimize engine dynamic performance.

关键词

Keywords

references

Views

417

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Model and Simulation of Aeroengine Load Spectrum Related to Operation

Simulation on hydromechanical controller of modern aero-engine

Modeling of and simulation research on turbofan engine based on MATLAB/SIMULINK

Start-up experimental research on oxidizer-rich preburner

Improvement on simulation software for static characteristics of liquid rocket engine

Related Author

SONG Ying-dong

SUN Zhi-gang

XU Min

WANG Xi

ZENG De-tang

XUE Min-dong

XIA Fei

HUANG Jin-quan

Related Institution

Nanjing University of Aeronautics and Astronautics

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

School of Astronautics, Beijing University of Aeronautics and Astrnautics

School of Astronautics, Beijing Univ.of Aeronautics and Astronautics

College of Energy & Power Engineering, Nanjing 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