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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    Title :

    LEAK DETECTION FOR PRESSURIZED FLUID SYSTEMS


    Additional title:

    LECKDETEKTION FÜR DRUCKFLUIDSYSTEME
    TECTION DE FUITE POUR SYST&#200


    Contributors:

    Publication date :

    2022-12-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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