Cryogenic fuels tanks (218, 220) for use in airfoil-shaped aircraft structures (1200) are disclosed herein. An example apparatus disclosed herein an airfoil-shaped structure (1200) disposed outboard of a fuselage of an aircraft (100). The example apparatus also includes a first cryogenic fuel tank (118) disposed inside the airfoil-shaped structure (1200).


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    Titel :

    Cryogenic fuel tanks for use in aircraft structures


    Weitere Titelangaben:

    Kryogene Treibstofftanks zur Verwendung in Flugzeugstrukturen
    Réservoirs de carburant cryogène pour utilisation dans structures d'avion


    Beteiligte:

    Erscheinungsdatum :

    06.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Cryogenic fuel tanks for use in aircraft structures

    BARMICHEV SERGEY D / SANKRITHI MITHRA M K V / STUHR VICTOR K | Europäisches Patentamt | 2016

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    Dix, Jr., E.H. / Mears, R.B. | Engineering Index Backfile | 1940


    Aluminum Aircraft Fuel Tanks

    Dix, E. H. / Mears, R. B. | SAE Technical Papers | 1940