A vertical or short takeoff and landing (V/STOL) aerial vehicle comprising: a wing having a leading edge and a trailing edge; a thrust rotor operatively coupled with the wing; and a lift rotor operatively coupled with the wing. The thrust rotor may comprise a first propeller having a first fixed axis of rotation that is substantially horizontal. The first propeller may be positioned forward of the leading edge. The lift rotor may comprise a second propeller having a second fixed axis of rotation that is substantially perpendicular to said first fixed axis of rotation. The wing may be operatively coupled with a fuselage.


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    Titel :

    Double-Blown Wing Vertical Takeoff and Landing Aircraft


    Beteiligte:
    ST CLAIR RAN D (Autor:in) / PARKS ROBERT W (Autor:in) / ORMISTON ROBERT (Autor:in)

    Erscheinungsdatum :

    14.06.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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