Aircraft turbine engine control systems development: Historical Perspective

被引：0

作者：

Lutambo, Jackson ^{[1
]}

Wang, Jiqiang ^{[1
,2
]}

Yue, Hong ^{[3
]}

Dimirovsky, Georgi ^{[4
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Jiangsu, Peoples R China

[2] AVIC Shenyang Engine Design & Res Inst, Shenyang 110015, Peoples R China

[3] Univ Strathclyde, Glasgow, Lanark, Scotland

[4] Dogus Univ Istanbul, Istanbul, Turkey

来源：

2015 34TH CHINESE CONTROL CONFERENCE (CCC) | 2015年

关键词：

Control system; Gas Turbine Engine; Hydromechanical System; FullAuthority Digital Electronic Control (FADEC); Digital Electronic Engine Control (DEEC);

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper describes the development of aircraft turbine engine control systems from the historical point of view to the present. With the increasing emphasis on aircraft safety, enhanced performance, and affordability, as well as the need to reduce the environmental effect caused by aircraft, there are many new challenges being faced by the designers of aircraft propulsion systems. The paper provides an overview of the various technological development activities in aircraft engine control and diagnostics, both current and some accomplished in the recent past. The motivations for each of the research efforts, the research approach, technical challenges, and the key progress to date are summarized.

引用

页码：5736 / 5741

页数：6

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