A dispenser of cooled or heated liquid which in one embodiment is a server cart for an aircraft. To avoid the need for a pump, the reservoir has a cooling or heating heat exchanger that helically coils around the main reservoir, which cools from the top down or heats from the bottom up, forming a counter current. The reservoir is connected to at least two conduits, one near the cooler top of the reservoir and one near the relatively warmer bottom of the reservoir. The two conduits connect to one another at a distance from the reservoir forming a dispensing passage, thereby allowing fluid to constantly circulate through the dispensing passage due to difference in the specific gravity in the fluid caused by the temperature difference. The elimination of the pump device is especially desirable for weight sensitive environments such as an aircraft.


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    Titel :

    DEVICE FOR PROVIDING A COOLED OR HEATED LIQUID ONBOARD AN AIRCRAFT


    Weitere Titelangaben:

    VORRICHTUNG ZUR BEREITSTELLUNG EINER GEKÜHLTEN ODER ERHITZTEN FLÜSSIGKEIT AN BORD EINES FLUGZEUGS
    DISPOSITIF POUR FOURNIR UN LIQUIDE REFROIDI OU CHAUFFE A BORD D'UN AVION


    Beteiligte:
    WITSCHKE MATTHIAS (Autor:in) / EBIGT WOLFGANG (Autor:in) / MUNDT MARCO (Autor:in) / DETJEN PETER (Autor:in)

    Erscheinungsdatum :

    21.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F24D DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS , Haus- oder Raumheizungssysteme, z.B. Zentralheizungssysteme / F24H FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, IN GENERAL , Erhitzer für flüssige oder gasförmige Stoffe, z.B. Wasser- oder Lufterhitzer mit Vorrichtungen zur Wärmeerzeugung, allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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