The present invention provides an aerodynamic structure (1), in particular for an aircraft (10), comprising a leading edge (2) having an outer structure, wherein the outer structure comprises: a first layer (3); and a second layer (4) geometrically corresponding to the first layer (3); wherein the first layer (3) is positioned on an outside (5) of the outer structure, the outside (5) being exposed to a flowing fluid, and the second layer (4) is positioned on an inside of the outer structure; and wherein the second layer (4) has a higher ductility than the first layer (3). Further the present invention provides an aircraft comprising such an aerodynamic structure.


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    Title :

    AERODYNAMIC STRUCTURE AND AIRCRAFT


    Additional title:

    AERODYNAMISCHE STRUKTUR UND FLUGZEUG
    STRUCTURE AÉRODYNAMIQUE ET AÉRONEF


    Contributors:

    Publication date :

    2024-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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