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Theoretical proposal of the engine for hale unmanned aerial vehicles

Identifikátory výsledku

  • Kód výsledku v IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25510%2F18%3A39913841" target="_blank" >RIV/00216275:25510/18:39913841 - isvavai.cz</a>

  • Nalezeny alternativní kódy

    RIV/68407700:21260/18:00324815

  • Výsledek na webu

  • DOI - Digital Object Identifier

Alternativní jazyky

  • Jazyk výsledku

    angličtina

  • Název v původním jazyce

    Theoretical proposal of the engine for hale unmanned aerial vehicles

  • Popis výsledku v původním jazyce

    The turn of the first and second millennium brought development of many technologies. One of these technologies are unmanned aerial vehicles. Success in armies meant an expansion into the civil sector. Requirements for rapid installation into an armament and costs as low as possible meant the usage of current aircraft engines without any further modifications. Especially in an effort to achieve maximal altitude of the vehicle the engine without the modification could be a cause of unsuccessful effort of exploitation of vehicle´s options. Simple analyses of the vehicles and their current propulsion systems were found significant elements of their interconnections. Then the currently appropriate propulsion systems were assigned with a choice justification and its possible alternatives, hazards, various advantages and so on. Then a type of the engine which has not been fully utilized on these vehicles yet was theoretically designed. The point that this engine has not been fully utilized on these vehicles is precisely why it could bring new benefits to this area. It could even outweigh the advantages of the engines currently used on these vehicles and potentially replace some of them. This part of the theoretical engine design is the subject of this article.

  • Název v anglickém jazyce

    Theoretical proposal of the engine for hale unmanned aerial vehicles

  • Popis výsledku anglicky

    The turn of the first and second millennium brought development of many technologies. One of these technologies are unmanned aerial vehicles. Success in armies meant an expansion into the civil sector. Requirements for rapid installation into an armament and costs as low as possible meant the usage of current aircraft engines without any further modifications. Especially in an effort to achieve maximal altitude of the vehicle the engine without the modification could be a cause of unsuccessful effort of exploitation of vehicle´s options. Simple analyses of the vehicles and their current propulsion systems were found significant elements of their interconnections. Then the currently appropriate propulsion systems were assigned with a choice justification and its possible alternatives, hazards, various advantages and so on. Then a type of the engine which has not been fully utilized on these vehicles yet was theoretically designed. The point that this engine has not been fully utilized on these vehicles is precisely why it could bring new benefits to this area. It could even outweigh the advantages of the engines currently used on these vehicles and potentially replace some of them. This part of the theoretical engine design is the subject of this article.

Klasifikace

  • Druh

    D - Stať ve sborníku

  • CEP obor

  • OECD FORD obor

    50703 - Transport planning and social aspects of transport (transport engineering to be 2.1)

Návaznosti výsledku

  • Projekt

  • Návaznosti

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Ostatní

  • Rok uplatnění

    2018

  • Kód důvěrnosti údajů

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Údaje specifické pro druh výsledku

  • Název statě ve sborníku

    Transport Means : proceedings of the international scientific conference

  • ISBN

  • ISSN

    1822-296X

  • e-ISSN

    2351-7034

  • Počet stran výsledku

    5

  • Strana od-do

    811-815

  • Název nakladatele

    Kaunas University of Technology

  • Místo vydání

    Kaunas

  • Místo konání akce

    Trakai

  • Datum konání akce

    3. 10. 2018

  • Typ akce podle státní příslušnosti

    WRD - Celosvětová akce

  • Kód UT WoS článku