Torsion box of an aircraft stabilizing surface comprising a front spar (15), a rear spar (17), ribs (21) and upper and lower stiffened skins, in which at least one of said skins (31) is stiffened with a plurality of stringers (33, 43), preferably omega-shaped stringers, extending all of them along the full skin span, preferably in a "conical" distribution, and having a decreasing cross section towards the skin outer edge.


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    Titel :

    TORSION BOX FOR AN AIRCRAFT STIFFENED WITH NON-PARALLEL STRINGERS


    Weitere Titelangaben:

    MIT NICHT PARALLELEN BÄNDERN VERSTEIFTE HÜLLE EINER TORSIONSBOX FÜR FLUGZEUGE
    REVÊTEMENT DE CAISSON DE TORSION POUR AVION RIGIDIFIÉ PAR DES LISSES NON PARALLÈLES



    Erscheinungsdatum :

    07.03.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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