DocumentCode
3091300
Title
Electronic starting control unit for small jet engine
Author
Dub, Michal ; Bajer, Josef ; Stepanek, Marcel
Author_Institution
Univ. of Defence, Brno, Czech Republic
fYear
2015
fDate
19-21 May 2015
Firstpage
1
Lastpage
4
Abstract
The article deals with small aircraft turbine engine ignition and electrical system. Theoretical part describes design of electronic control unit based on analysis of engine starting process. Experimental part presents construction of second prototype of electronic control unit. Experimental results are discussed including graphical presentation of engine parameters.
Keywords
aerospace control; ignition; jet engines; starting; electrical system; electronic starting control unit; engine parameter graphical presentation; small aircraft turbine engine ignition; small jet engine starting process analysis; Aerospace electronics; Aircraft propulsion; Ignition; Microcontrollers; Turbines; aircraft propulsion; electronic circuits; microprocessors;
fLanguage
English
Publisher
ieee
Conference_Titel
Military Technologies (ICMT), 2015 International Conference on
Conference_Location
Brno
Print_ISBN
978-8-0723-1976-3
Type
conf
DOI
10.1109/MILTECHS.2015.7153748
Filename
7153748
Link To Document