A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID VTOL VEHICLE


    Beteiligte:
    EGAN JAMES C (Autor:in) / EGAN JOEL D (Autor:in)

    Erscheinungsdatum :

    2016-05-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft



    HYBRID VTOL VEHICLE

    EGAN JAMES C / EGAN JOEL D | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID VTOL VEHICLE

    JAMES C EGAN / JOEL D EGAN | Europäisches Patentamt | 2019

    Freier Zugriff

    Hybrid VTOL vehicle

    EGAN JAMES C / EGAN JOEL D | Europäisches Patentamt | 2018

    Freier Zugriff

    Hybrid VTOL vehicle

    EGAN JAMES C / EGAN JOEL D | Europäisches Patentamt | 2018

    Freier Zugriff

    Hybrid vtol vehicle

    EGAN JAMES C / EGAN JOEL D | Europäisches Patentamt | 2016

    Freier Zugriff