A water supply system for an aircraft has water lines which lead to a consumer group with at least one water consumer and at least one buffer upstream of the at least one water consumer. A discharge line discharges water from a water tank into the water lines and a feed pump in the discharge line supplies water from the water tank into the water lines. Each of the water lines is a flexible hose made of plastic with an internal diameter of at least 4 mm and a length of at most 100 m, and the feed pump is configured to convey water from the water tank into the water lines at a pressure of at most 25 bar and a flow rate of at most 1.4 liters per minute.


    Access

    Download


    Export, share and cite



    Title :

    WATER SUPPLY SYSTEM FOR AN AIRCRAFT, AND AIRCRAFT WITH THE WATER SUPPLY SYSTEM


    Contributors:

    Publication date :

    2023-05-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    E03B Anlagen oder Verfahren zum Gewinnen, Sammeln oder Verteilen von Wasser , INSTALLATIONS OR METHODS FOR OBTAINING, COLLECTING, OR DISTRIBUTING WATER / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT WATER SUPPLY SYSTEM

    MURAYAMA HIROSHI | European Patent Office | 2022

    Free access

    Aircraft water supply system

    MURAYAMA HIROSHI | European Patent Office | 2024

    Free access

    Aircraft water supply system

    MURAYAMA HIROSHI | European Patent Office | 2022

    Free access

    Water supply system for an aircraft, and aircraft with the water supply system

    KESSLER ROLF / SCHÄFER PHILIPP / PHILIPP JAN BORIS | European Patent Office | 2024

    Free access

    AIRCRAFT WATER SUPPLY SYSTEM

    MURAYAMA HIROSHI | European Patent Office | 2022

    Free access