• DocumentCode
    2260068
  • Title

    Aircraft turbine engine control systems development: Historical perspective

  • Author

    Lutambo, Jackson ; Wang, Jiqiang ; Yue, Hong ; Dimirovsky, Georgi

  • Author_Institution
    Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    5736
  • Lastpage
    5741
  • Abstract
    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.
  • Keywords
    DVD; Decision support systems; Control system; Digital Electronic Engine Control (DEEC); FullAuthority Digital Electronic Control (FADEC); Gas Turbine Engine; Hydromechanical System;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7260534
  • Filename
    7260534