A chiller assembly for a galley having one or more rectangular galley compartments defined by a back wall, a floor, a top wall and two opposing side walls, the chiller assembly comprising a chiller system comprising a heat exchanger configured to be located in use in a space adjacent a side wall of a compartment external to the compartment, and a blower duct connected to receive chilled air from the heat exchanger, the blower duct arranged to extend adjacent the top wall or the floor of the compartment, the blower duct having vents to blow chilled air into the compartment via the top wall or the floor, the chiller system further comprising a return duct arranged adjacent the other of the floor or the top wall of the compartment to suck air from the compartment and return it to the heat exchanger.


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    Title :

    AIRCRAFT CHILLING SYSTEM ARCHITECTURE


    Contributors:

    Publication date :

    2024-07-18


    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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