This disclosure generally relates to lightweight thermionic microengines for aerial vehicles. The aerial vehicles include a propulsion system. The propulsion system includes a combustor. The propulsion system further includes a thermionic generator that receives heat from the combustor and generates electricity. The propulsion system further includes one or more propulsion motors that receive the electricity generated by the thermionic generator. The propulsion motors may provide power to one or more propellers to generate lift and thrust for a UAV.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LIGHTWEIGHT THERMIONIC MICROENGINES FOR AERIAL VEHICLES


    Beteiligte:
    GHOSHAL ANKITA (Autor:in)

    Erscheinungsdatum :

    14.03.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H10N / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Lightweight thermionic microengines for aerial vehicles

    GHOSHAL ANKITA | Europäisches Patentamt | 2018

    Freier Zugriff

    Lightweight thermionic microengines for aerial vehicles

    GHOSHAL ANKITA | Europäisches Patentamt | 2020

    Freier Zugriff

    Designing Microengines for Reliability

    Hirtz, N. | British Library Conference Proceedings | 1997


    Study on measurement technology of microengines [5253-55]

    Guan, L. / Wang, J. / Chen, D. et al. | British Library Conference Proceedings | 2003


    Designing and Operating Electrostatically Driven Microengines

    Rodgers, M. S. / Sniegowski, J. / Miller, S. et al. | British Library Conference Proceedings | 1998