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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    Title :

    Structural component for an aircraft or spacecraft


    Additional title:

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



    Publication date :

    2018-05-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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