The present invention relates to a rotary flapping-wing flight apparatus having rotary wings, which flap at both sides of a fuselage of the flight apparatus through dual rotation for simultaneously revolving and rotating in the circulation direction of the inner middle, center top, outer middle and center bottom ends thereof, almost stand upright to perform upward flapping to be lifted without fluid resistance when the wings are passing the inner middle end thereof, and are almost horizontally spread out to perform downward flapping while pushing fluid in the vertical downward direction, when the wings are passing the outer middle end thereof.


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    Titel :

    ROTARY FLAPPING-WING FLIGHT APPARATUS FOR VERTICAL LIFT AND HORIZONTAL DESCENT


    Weitere Titelangaben:

    DREHFLÜGELFLUGVORRICHTUNG FÜR VERTIKALEN AUFTRIEB UND HORIZONTALEN ABSTIEG
    APPAREIL DE VOL À AILES BATTANTES ROTATIVES POUR PORTANCE VERTICALE ET DESCENTE À L'HORIZONTALE


    Beteiligte:
    LEE SANG CHEOL (Autor:in)

    Erscheinungsdatum :

    27.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



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