Disclosed is an aircraft having ducted fans inside ducts that are incorporated into an aircraft body design to configure an undercambered bottom. Two forward ducts intake above the body (creating lift) and expel air downward and slightly outward at the front of the craft. Two rear ducts also intake above the body, but expel air downwardly and outwardly at the rear of the craft. The overall volume and footprint for the craft enables use in existing parking and other environmental structures normally used to accommodate automobiles.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    VERTICAL TAKE-OFF OR LANDING (VTOL) AERIAL DEVICE


    Beteiligte:
    STUKAS KAYLEE (Autor:in)

    Erscheinungsdatum :

    2021-10-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Vertical take-off or landing (VTOL) aerial device

    STUKAS KAYLEE | Europäisches Patentamt | 2023

    Freier Zugriff

    VTOL (vertical take-off and landing) UAV (unmanned aerial vehicle)

    ZHANG JIE / YU CHUNGUANG / LIU ZHUOBIN et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    STRUCTURAL FEATURES OF VERTICAL TAKE-OFF AND LANDING (VTOL) AERIAL VEHICLE

    HUANG DENG | Europäisches Patentamt | 2023

    Freier Zugriff


    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

    MOORE ANDREW DUDLEY / WILSON JOHN | Europäisches Patentamt | 2022

    Freier Zugriff