A galley cooling system for an aircraft includes a trolley compartment which includes a cooling unit. A first cooling fluid manifold connects to a cooling fluid outlet or a cooling fluid inlet and has a first cooling fluid manifold wall defining a portion of a lateral boundary of a receiving space of the trolley compartment. A first cooling fluid opening is in the first cooling fluid manifold wall connecting the first cooling fluid manifold to the receiving space of the trolley compartment. A second cooling fluid manifold connected to the cooling fluid inlet or outlet of the cooling unit has a second cooling fluid manifold wall defining a portion of an upper boundary of the receiving space of the trolley compartment, a second cooling fluid opening in the second cooling fluid manifold wall to connect the second cooling fluid manifold to the receiving space of the trolley compartment.


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    Titel :

    Galley cooling system and method of operating a galley cooling system


    Beteiligte:

    Erscheinungsdatum :

    27.08.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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