• DocumentCode
    1661331
  • Title

    LV100 gas turbine control: a case study

  • Author

    Ravi, R. ; Minto, K.D.

  • Author_Institution
    Control Syst. & Electron. Technol. Lab., Gen. Electr. Corp. Res. & Dev., Schenectady, NY, USA
  • Volume
    2
  • fYear
    1994
  • Firstpage
    1598
  • Abstract
    The subject of this case study is the LV100, a relatively new turbine engine targeted at land-based applications, specifically as the main propulsion unit in the next generation of armored vehicles. Because of its ground-based applications, the turbine is designed to run efficiently over a much larger range of operating points (speeds) than a corresponding aircraft engine would. A key element contributing to the success of the machine is the control system. While the present designs are within specifications, they are quite complicated. The focus of this study, therefore, is to bring to bear modern control design techniques to improving the control system. The paper describes in general terms the problem and the design specifications
  • Keywords
    control system analysis; control system synthesis; gas turbines; military equipment; propulsion; LV100 gas turbine control; armored vehicles; control system; design specifications; land-based applications; main propulsion unit; modern control design techniques; Computer aided software engineering; Control systems; Degradation; Engines; Process design; Shafts; Temperature control; Time factors; Turbines; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1994., Proceedings of the 33rd IEEE Conference on
  • Conference_Location
    Lake Buena Vista, FL
  • Print_ISBN
    0-7803-1968-0
  • Type

    conf

  • DOI
    10.1109/CDC.1994.411214
  • Filename
    411214