Fitting for aircrafts, comprising two angled pieces (1) joined to each other, each of them defining a first section (11) and a second section (12), an external plate (2) joined with both angled pieces (1), and a skin (3) joined to the external plate (2), the skin (3) being independent from the angled pieces (1).It permits to discharge the radius of the fitting angles defined by the angled pieces, discharging both angles, assuring than there is no rivet or similar joining elements installed in the angled pieces, assuring no ply continuity in the marked area.


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    Titel :

    FITTING FOR AIRCRAFTS


    Weitere Titelangaben:

    BESCHLAG FÜR FLUGZEUGE
    FERRURE POUR AÉRONEFS


    Beteiligte:

    Erscheinungsdatum :

    05.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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