A seal for sealing an aircraft fuel tank, an aircraft wing rib and stringer sealing assembly, an aircraft wing fuel tank, an aircraft structural wing box, an aircraft wing, and a method of sealing an aperture are disclosed. The seal is for sealing a wing rib to a stringer passing through an aperture in the rib at a variable position in the aperture. The seal includes self-adjustment means to absorb any tolerance when forming the seal, upon the stringer being assembled into the aperture in the rib.


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    Titel :

    AIRCRAFT FUEL TANK APERTURE SEALING


    Beteiligte:
    EDWARDS PAUL (Autor:in) / PEACOCK ANTONY (Autor:in) / SANDERSON TIMOTHY (Autor:in)

    Erscheinungsdatum :

    03.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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