An aircraft potable water system (20) comprises outlet facilities (30) and a recirculation path (40) that supplies potable water thereto. The system (20) can operate in a high-usage condition whereat recirculation through path (40) is temporarily interrupted, thereby permitting supply water pressure to remain relatively high despite water being quickly tapped therefrom.

    Un système deau potable pour aéronef (20) comprend des installations de sortie (30) et un circuit de recirculation (40) qui assure lapprovisionnement en eau potable. Le système (20) peut fonctionner dans des conditions de grande utilisation, alors que la recirculation par le circuit (40) est temporairement interrompue. Cela permet à la pression deau de distribution de demeurer relativement élevée, même si leau est récoltée rapidement.


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    Title :

    AIRCRAFT POTABLE WATER SYSTEM


    Additional title:

    SYSTEME D'EAU POTABLE POUR AERONEF


    Contributors:
    HARR JOHN (author) / LEI MARTIN (author) / MACKULIN BRYAN (author)

    Publication date :

    2018-08-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet



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