A leading-edge device for an aerodynamic component is disclosed having a first skin element having an inner surface and an aerodynamic outer surface, and further includes a second skin element having an inner surface and an aerodynamic outer surface. The leading-edge device includes a first coupling element protruding from the inner surface of the first skin element and a second coupling element protruding from the inner surface of the second skin element. The first and second coupling elements are coupled to each other in a coupling region. The first skin element and the first coupling element are formed as a single-piece structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LEADING EDGE DEVICE FOR AN AERODYNAMIC COMPONENT AND METHOD FOR MANUFACTURING A LEADING-EDGE DEVICE FOR AN AERODYNAMIC COMPONENT


    Beteiligte:
    FEES MARTIN (Autor:in) / BAST CHRISTIAN (Autor:in) / LANGE ROBERT (Autor:in) / JOACHIM LILIAN (Autor:in)

    Erscheinungsdatum :

    27.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LEADING EDGE DEVICE FOR AN AERODYNAMIC COMPONENT AND METHOD FOR MANUFACTURING A LEADING-EDGE DEVICE FOR AN AERODYNAMIC COMPONENT

    FEES MARTIN / BAST CHRISTIAN / LANGE ROBERT et al. | Europäisches Patentamt | 2025

    Freier Zugriff



    Aerodynamic and Acoustic Design of Silent Leading Edge Device

    Pott-Pollenske, Michael / Wild, Jochen W. / Bertsch, Lothar | AIAA | 2014


    Leading edge buckling due to aerodynamic heating

    Mansfield, Eric Harold | SLUB | 1960