An aircraft potable-water system (10) comprising an automatic valve (60) associated with an overflow line (50) and an automatic switch (70) associated with the storage tank (30). The switch (70) vents the storage tank (30) when it is not full, and automatically converts to a tank-pressurizing condition when the storage tank (30) is full. This conversion of the switch (70) causes the valve (60) to move to an overflow-open position so that excess potable water can be drained through the drainmast (18).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft potable-water system


    Beteiligte:

    Erscheinungsdatum :

    25.10.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT POTABLE WATER SYSTEM

    HARR JOHN / LEI MARTIN / MACKULIN BRYAN | Europäisches Patentamt | 2018

    Freier Zugriff

    21st Century Aircraft Potable Water Systems

    Thorpe, George W. | SAE Technical Papers | 1999


    21st Century Aircraft Potable Water Systems

    Thorpe, G. W. / Society of Automotive Engineers | British Library Conference Proceedings | 1999


    Cart Compartment Cooling Using Aircraft Potable Water

    PUCKER ANDREW L / MORAN THOMAS JOSEPH / MOVSESIAN SAMI | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRCRAFT WITH A POTABLE WATER SYSTEM AND INSTALLATION METHOD

    ALBERS FREDERIK / HEGENBART MATTHIAS / BOENNING KENNETH et al. | Europäisches Patentamt | 2025

    Freier Zugriff