An aircraft wing (308) including a fuel tank (314) located in the wing (308), a channel (336) defining a cavity (313) in the fuel tank (314), the channel (336) including at least two channel ends terminating at an upper or lower wing surface (340, 342), a driveshaft (316) located in the cavity (313); and an access panel (390) located on the wing surface (340, 342) and being movable between an open position so that access to the cavity (313) is permitted, and a closed position so that the cavity (313) is at least partially covered by the access panel (390) to inhibit access to the cavity (313).


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    Titel :

    CROSS-WING DRIVESHAFT CHANNEL


    Weitere Titelangaben:

    ANTRIEBSKANAL IN FLÜGELLÄNGSRICHTUNG
    CANAL TRANSVERSAL AILAIRE POUR ARBRE DE TRANSMISSION


    Beteiligte:
    IVANS STEVEN (Autor:in) / ANDERSON ADAM (Autor:in)

    Erscheinungsdatum :

    28.11.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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