In accordance with at least one aspect of this disclosure, a fluid system (200) of an aircraft includes a primary fluid conduit (201) that conveys a primary fluid, and a leak detection system (250) disposed around at least a portion of the primary fluid conduit (201) and forming one or more detection volumes (251a). The leak detection system (250) determines whether there is a primary fluid leak into the one or more detection volumes (251a) by sensing a pressure change in the one or more detection volumes (251a).


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    Titel :

    LEAK DETECTION FOR PRESSURIZED FLUID SYSTEMS


    Weitere Titelangaben:

    LECKDETEKTION FÜR DRUCKFLUIDSYSTEME
    TECTION DE FUITE POUR SYST&#200


    Beteiligte:

    Erscheinungsdatum :

    14.12.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02M Zuführen von Brennstoff-Luft-Gemischen oder deren Bestandteilen bei Brennkraftmaschinen allgemein , SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF



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