• DocumentCode
    35438
  • Title

    Electric Starter Generators: Their Integration into Gas Turbine Engines

  • Author

    Bhangu, Bikramjit S. ; Rajashekara, Kaushik

  • Author_Institution
    Adv. Technol. Centre, Rolls-Royce Singapore, Singapore, Singapore
  • Volume
    20
  • Issue
    2
  • fYear
    2014
  • fDate
    March-April 2014
  • Firstpage
    14
  • Lastpage
    22
  • Abstract
    THE MARKET FOR INTEGRATED power systems for more electric aircrafts and, in particular, for unmanned air vehicles (UAVs) is rapidly developing [1]. Due to space constraints, a practical solution for UAVs is to employ electric-starter generators (ESGs) embedded in gas turbine engines to facilitate electric engine crank, assist the engine in reaching the desired idle speed, generate power to drive the onboard auxiliaries, and improve the overall efficiency of the system [2]. To control the ESG, a position sensor is required for the closed-loop control of speed and torque. However, the traditional sensors that provide accurate knowledge of the machine rotor position to facilitate precise control of the ESG cannot be used because of adverse operating conditions.
  • Keywords
    aerospace engines; autonomous aerial vehicles; closed loop systems; rotors; closed-loop control; electric aircrafts; electric starter generators; gas turbine engines; integrated power systems; machine rotor position; onboard auxiliaries; position sensor; space constraints; unmanned air vehicles; Aerospace electronics; Gas turbines; Permanent magnets; Power electronics; Torque control; Turbines; Unmanned aerial vehicles;
  • fLanguage
    English
  • Journal_Title
    Industry Applications Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    1077-2618
  • Type

    jour

  • DOI
    10.1109/MIAS.2013.2288398
  • Filename
    6690204