An aircraft galley plumbing system includes a potable water sub-system, a waste water sub-system, and a valve in fluid communication with the potable water sub-system and the waste water sub-system. The potable water sub-system includes a plurality of potable water supply lines configured to provide potable water from a potable water source to at least one galley installation. The waste water sub-system includes a plurality of drain lines configured to receive waste water from the at least one galley installation, a plurality of waste water sumps configured to receive waste water from the plurality of drain lines, and a main drain line. The potable water sub-system is configured to be filled from the potable water source when the valve is in a first operational configuration. The potable water sub-system is configured to empty into the waste water sub-system via the valve when the valve is in a second operational configuration.


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    Title :

    Aircraft Galley Plumbing System


    Contributors:

    Publication date :

    2021-02-04


    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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