An aircraft fluid tank module (10) comprises a pressure-free tank shell (12) having an outer surface (18), a contour of which is adjusted to a contour of an installation space provided on board an aircraft for installation of the aircraft fluid tank module (10), and at least one fastening device (34) adapted to fasten the aircraft fluid tank module (10) to a primary structure element of an aircraft.


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    Title :

    AIRCRAFT PROVIDED WITH A FLUID TANK MODULE


    Additional title:

    FLUGZEUG UMFASSEND EIN FLÜSSIGKEITSBEHÄLTERMODUL
    AÉRONEF COMPRENANT UN MODULE DE RÉSERVOIR DE FLUIDE


    Contributors:

    Publication date :

    2018-10-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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