A mult-rib box-shaped aeronautical structure comprising upper and lower skins (19, 21) stiffened by span wise stringers (25, 25', 25"), span wise front and rear spars (11, 13) and chord wise ribs (27, 27', 27"), where at least one panel (31, 33) of any of said skins (19, 21) is non delimited by said ribs (27, 27', 27") and said stringers (25, 25', 25") and comprise an stiffening element (41, 43) arranged as a panel breaker to avoiding the need of increasing the panel thickness to withstand buckling loads.


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    Titel :

    An aircraft lifting surface skin


    Weitere Titelangaben:

    Flugzeugtragflächenhaut
    Peau de surface portante d'un avion



    Erscheinungsdatum :

    31.05.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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