An aircraft wing torsion box (100) is provided, the aircraft wing torsion box having a front associated with a leading portion of the wing torsion box and a rear associated with a trailing portion of the wing torsion box, the wing torsion box comprising: a support member (101) comprising a front spar (102) and a rear spar (103) and a connecting portion (106,104,108,105,107) between the front and rear spars, the connecting portion comprising at least one interposing spar (104,105), at least one portion of upper wing skin (120) ; and at least one portion of lower wing skin (130), at least one portion of the upper wing skin and at least one portion of the lower wing skin being supported by the support member.


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    Titel :

    AIRCRAFT WING TORSION BOX, AIRCRAFT WING AND AIRCRAFT


    Weitere Titelangaben:

    FLUGZEUGFLÜGEL TORSIONSBOX, FLUGZEUGFLÜGEL UND FLUGZEUG
    CAISSON DE TORSION POUR VOILURE D'AERONEF, VOILURE D'AERONEF ET AERONEF


    Beteiligte:
    EVANS STEVEN (Autor:in)

    Erscheinungsdatum :

    01.05.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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