According to the present invention, a variable span morphing wing comprises: a driving unit provided to an aircraft fuselage to generate a rotational force; a scissors unit composed of a plurality of steps to enable one end to receive the rotational force from the driving unit to enable a length to be varied in a longitudinal direction; an auxiliary wing coupled to an other end of the scissors unit to be moved in the longitudinal direction of the wing in accordance with a length change of the scissors unit; and a main wing coupled to the aircraft fuselage to receive the auxiliary wing therein. Moreover, the present invention is capable of performing various tasks based on a modification of a flexible shape in a different aerodynamic condition.


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    Titel :

    VARIABLE SPAN MORPHING WING


    Beteiligte:
    BAE JAE SUNG (Autor:in) / HWANG JAI HYUK (Autor:in) / CHOI SOO MIN (Autor:in)

    Erscheinungsdatum :

    23.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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