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
         
        
        
        
        
        
            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;
         
        
        
        
            Conference_Titel : 
Pulsed Power Conference (PPC), 2011 IEEE
         
        
            Conference_Location : 
Chicago, IL
         
        
        
            Print_ISBN : 
978-1-4577-0629-5
         
        
        
            DOI : 
10.1109/PPC.2011.6191401