System for remotely measuring pressure for pressures exerted by a fluid (2) conveyed by a pipe (1), the system comprising a measuring tube (3) with a first end (4) connected to the pipe (1) and a second end (5) to a pressure sensing element (6). The measuring tube (3) completely filled with a liquid (7) and comprising watertight membranes that respectively close its both ends (4, 5) retaining the liquid (7) inside it, a first membrane (8) in contact with the fluid (2) and closing its first end (4), and a second membrane (9) in contact with the pressure sensing element (6) and closing its second end (5). The first membrane (8) being sensitive to fluid (2) pressure oscillations and the second membrane (9) to liquid (7) pressure oscillations for propagating the pressure exerted by the fluid (2) to the pressure sensing element (6) for its measure.


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    Titel :

    Aircraft fuel tank comprising a system for remotely measuring pressure


    Weitere Titelangaben:

    Flugzeugkraftstofftank mit einem System zur entfernten Druckmessung
    Réservoir de carburant d'aéronef avec un système de mesure de pression à distance


    Beteiligte:

    Erscheinungsdatum :

    2018-10-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE



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