The invention relates to an integrated multispar torsion box structure of composite material for aircraft, comprising a lower skin (12), an upper skin (11), several spars (9), each of which comprises in turn a chord (13) and a web (14), several stringers (10) in the lower skin (12) and several stringers (10) in the upper skin (11), characterized in that the mentioned integrated torsion box structure is achieved by means of joining unitary U-shaped structural elements (15), unitary U-shaped structural elements (16) with a flap and unitary C-shaped structural elements (17) with a flap. The invention also relates to a method for manufacturing an integrated multispar torsion box structure of composite material for aircraft.


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    Titel :

    MULTISPAR TORSION BOX MADE FROM COMPOSITE MATERIAL


    Weitere Titelangaben:

    AUS VERBUNDWERKSTOFF HERGESTELLTER TORSIONSKASTEN MIT MEHREREN HOLMEN
    CAISSON DE TORSION MULTI-LONGERONS INTÉGRÉ EN MATÉRIAU COMPOSITE



    Erscheinungsdatum :

    2016-10-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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