An aircraft fuel tank access cover comprises an inner door, an outer door and a clamping arrangement for clamping the doors together about an access aperture in the skin of the fuel tank. The clamping arrangement comprises a bolt in-molded in a generally central part of the inner door and or external nut. The doors have reinforcing rib arrangements to spread the clamping load to the peripheral edges thereof.


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    Titel :

    Aircraft fuel tank access cover and an aircraft fuel tank


    Beteiligte:

    Erscheinungsdatum :

    24.11.2015


    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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