The present invention relates to a structural component for an aircraft or spacecraft having an outer skin 10, comprising at least one former element 12 for reinforcing the outer skin 10. The former element 12 is arcuately curved in accordance with an inner contour of the outer skin 10, wherein the former element 12 has a plurality of first cutouts 15 for receiving longitudinal reinforcements 16 and at least one second cutout 20, which is configured between adjacent first cutouts 15 of one or more former elements 12. The invention furthermore relates to an aircraft or spacecraft with the structural component according to the invention.


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    Titel :

    Structural component for an aircraft or spacecraft


    Weitere Titelangaben:

    Strukturkomponente für ein Flugzeug oder Raumfahrzeug
    Élément structurel pour aéronef ou engin spatial


    Beteiligte:

    Erscheinungsdatum :

    16.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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