The present invention pertains to a structural component (1) for reinforcing the fuselage (6) of an aircraft or spacecraft, wherein the structural component (1) is integrally formed and segmented into surface-like stiffening sections, whereby at least one stiffening section is formed as a rigid mesh section (2), and at least one stiffening section is formed as a solid section (3). The present invention further pertains to a method for producing a structural component of this type.


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    Titel :

    Structural component and method for producing a structural component


    Weitere Titelangaben:

    Strukturkomponente und Verfahren zur Herstellung einer Strukturkomponente
    Composant structurel et procédé de fabrication associé


    Beteiligte:
    SAUER MICHAEL (Autor:in) / TIRYAKI MEMIS (Autor:in)

    Erscheinungsdatum :

    11.05.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS



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