An intermeshing rotary-wing aircraft comprises a first rotary blade portion including a first blade and a second blade, a second rotary blade portion including a third blade and a fourth blade, a first shaft and a second shaft that transmit power to the first rotary portion and the second rotary portion and are symmetrically positioned at a predetermined angle, a first swash plate portion for controlling the first blade and the second blade, and a second swash plate portion for controlling the third blade and the fourth blade, wherein the first swash plate is coupled to three linkages, in which the coupled positions are located at the vertices of an equilateral triangle, the second swash plate has the same shape as the first swash plate, and the two equilateral triangles of the first swash plate and the second swash plate are star-shaped when horizontally moved and overlapped.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    INTERMESHING ROTARY-WING AIRCRAFT WITH SYMMETRICAL SWASH PLATE


    Beteiligte:
    KIM TAESAN (Autor:in)

    Erscheinungsdatum :

    2019-06-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING



    INTERMESHING ROTARY-WING AIRCRAFT WITH SYMMETRICAL SWASH PLATE

    KIM TAESAN | Europäisches Patentamt | 2018

    Freier Zugriff

    INTERMESHING ROTOR HELICOPTER BY USING SWASH PLATE

    KIM TAE SAN | Europäisches Patentamt | 2018

    Freier Zugriff

    INTERMESHING ROTOR HELICOPTER BY USING SWASH PLATE

    KIM TAE SAN | Europäisches Patentamt | 2016

    Freier Zugriff