Document Type : Scientific extension

Authors

1 Assistant Professor, Faculty of Mechanical Engineering, Malek Ashtar University of Technology, Shahin Shahr, Esfahan, Iran

2 M.Sc. Student, Faculty of Mechanical Engineering, Malek Ashtar University of Technology, Esfahan, Iran

3 M.Sc. Holder, Faculty of Mechanical Engineering, Malek Ashtar University of Technology, Shahin Shahr, Esfahan, Iran.

Abstract

The performance of the propulsion system and the engine, known as the heart of the aircraft, is highly dependent on subsystems, such as the engine control subsystem.Today, most modern military and civil aircraft use turbine engines to generate thrust. The engine control system is one of the most challenging aircraft control systems that has undergone significant changes and improvements over time. The goal of any engine control system is to provide maximum performance in each flight conditions. With the increase in requirements and the development of technology in propulsion systems, digital electronic engine control and full authority digital engine (electronics) control have replaced hydromechanical control. The purpose of this study is to present the development process of turbine engine control system historically and to find new methods of engine control. Depending on the complexity of the aircraft propulsion system engine, the engine control approach will be determined and designed.

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Main Subjects

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