• DocumentCode
    1944969
  • Title

    Fast pulser for high-altitude ignition research

  • Author

    Roth, Ian S. ; Planck, Peter Ver ; Gaudreau, Marcel P J ; Kempkes, Michael A.

  • Author_Institution
    Diversified Technol., Inc., Bedford, MA, USA
  • fYear
    2011
  • fDate
    19-23 June 2011
  • Firstpage
    131
  • Lastpage
    134
  • Abstract
    A jet engine can flame out at high altitude because the igniter cannot couple enough energy into the low-pressure air-fuel mixture. To reignite the engine, the aircraft must descend to a lower altitude where the air pressure is higher. Under a recent U.S. Air Force SBIR grant, Diversified Technologies, Inc. designed and built a fast ignition pulser. The pulser was delivered to the Air Force Research Laboratory for testing to determine the optimum parameters for high-altitude jet ignition. The pulser, based on magnetic pulse compression, is immune to arcs at the output. It delivers a pulse at 27 kV and 37 mJ with a rise-time of 17 ns at a pulse rate of 8 kHz. The overall efficiency is 38%. This paper discusses the design and performance of the laboratory pulser.
  • Keywords
    electric ignition; jet engines; military aircraft; Air Force Research Laboratory; Diversified Technologies, Inc; U.S. Air Force SBIR grant; air pressure; aircraft; fast ignition pulser; high-altitude ignition research; jet engine; low-pressure air-fuel mixture; magnetic pulse compression; Capacitance; Capacitors; Ignition; Inductance; Insulated gate bipolar transistors; Laboratories; Magnetic cores;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Pulsed Power Conference (PPC), 2011 IEEE
  • Conference_Location
    Chicago, IL
  • ISSN
    2158-4915
  • Print_ISBN
    978-1-4577-0629-5
  • Type

    conf

  • DOI
    10.1109/PPC.2011.6191401
  • Filename
    6191401