Electronic Starting Control Unit for Small Jet Engine
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F15%3A00531305" target="_blank" >RIV/60162694:G43__/15:00531305 - isvavai.cz</a>
Result on the web
<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2015.7153748" target="_blank" >10.1109/MILTECHS.2015.7153748</a>
Alternative languages
Result language
angličtina
Original language name
Electronic Starting Control Unit for Small Jet Engine
Original language description
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.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
KA - Militarism
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
International Conference on Military Technologies 2015
ISBN
978-80-7231-976-3
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
593-596
Publisher name
University of Defence
Place of publication
Brno
Event location
Brno
Event date
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Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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