AN AIRPLANE WITH TANDEM ROTO-STABILIZERS The present invention relates to an airplane capable of hyper-short / vertical takeoff and landing (hyper-STOL / VTOL) and having non-rotatable vertical propulsions. It 5 attempts to overcome a limitation of QuadPlane design by making efficient use of both horizontal and vertical propulsions during hovering and vertical flight. Most Illustrative Diagram: FIG. 2 co <~ C) C)


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    Titel :

    AN AIRPLANE WITH TANDEM ROTO-STABILIZERS


    Beteiligte:
    POH CHUNG-KIAK (Autor:in) / POH CHUNG-HOW (Autor:in)

    Erscheinungsdatum :

    26.08.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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