Embodiments disclosed herein relate to electroaerodynamic (EAD) thrusters for use in thrust generation. An EAD thruster may include one or more ion sources, one or more ion collectors, and one or more airfoils. In some embodiments, the one or more of the one or more ion sources and/or ion collectors may be integrated into a surface of the one or more airfoils. The EAD thruster arrangement may also include multiple EAD stages in some embodiments.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SURFACE-INTEGRATED ELECTROAERODYNAMIC THRUSTERS


    Beteiligte:
    BARRETT STEVEN (Autor:in) / XU HAOFENG (Autor:in) / BROWN ARTHUR (Autor:in) / GOMEZ VEGA NICOLAS (Autor:in) / PEROVICH NICOLAS (Autor:in)

    Erscheinungsdatum :

    12.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    DUCTED ELECTROAERODYNAMIC THRUSTERS

    BARRETT STEVEN / XU HAOFENG / BROWN ARTHUR et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Empirical Study of Ground Proximity Effects for Small-scale Electroaerodynamic Thrusters

    Nations, Grant / Nelson, C. Luke / Drew, Daniel S. | ArXiv | 2023

    Freier Zugriff

    Model of Multistaged Ducted Thrusters for High-Thrust-Density Electroaerodynamic Propulsion

    Gomez-Vega, Nicolas / Brown, Arthur / Xu, Haofeng et al. | AIAA | 2023



    ELECTROAERODYNAMIC DEVICES

    BARRETT STEVEN / XU HAOFENG / HE YIOU | Europäisches Patentamt | 2020

    Freier Zugriff