An aerodynamic component (10) which in particular is suitable for use in an aircraft comprises an outer skin sheet (12) having an inner surface and an outer surface and being provided with a plurality of perforation openings (14) allowing a flow of air therethrough. The outer surface of the outer skin sheet (12) forms an aerodynamic surface of the aerodynamic component (10). The aerodynamic component (10) further comprises a sandwich panel (18) which includes an outer layer (20) facing the inner surface of the outer skin sheet (12), an inner layer (22) facing away from the inner surface of the outer skin sheet (12) and a foam core (24) sandwiched between the outer layer (20) and the inner layer (22). The sandwich panel (18) is provided with a plurality of connection openings (26) extending through the sandwich panel (18) between the outer layer (20) and the inner layer (22) and allowing a flow of air therethrough.


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    Titel :

    Aerodynamic component and method for producing an aerodynamic component


    Weitere Titelangaben:

    Aerodynamisches Bauteil und Verfahren zur Herstellung eines aerodynamischen Bauteils
    Composant aérodynamique et procédé de fabrication d'un composant aérodynamique


    Beteiligte:
    TEICH BENJAMIN (Autor:in)

    Erscheinungsdatum :

    2018-09-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse



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