The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plurality of frames (17) with mouseholes for the passage of stringers (15) at their crossing zones. The reinforcing elements (51, 53) are configured with a suitable shape to be superimposed to the stringers (15) in said areas. The invention also provides manufacturing processes of said integrated aircraft structure (10).


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    Title :

    Aircraft structure with integrated reinforcing elements


    Additional title:

    Flugzeugstruktur mit integrierten Verstärkungselementen
    Structure d'aéronef avec éléments de renfort intégrés


    Contributors:

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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