A differential pressure sensor system (12) for use in an aircraft (10) comprises a differential pressure sensor (22) for determining a differential pressure between a pressurizable aircraft cabin (24) and an aircraft environment (20), the differential pressure sensor (22) having a first port (26) connectable to the pressurizable aircraft cabin (24) via a first line (30) and a second port (28) connectable to the aircraft environment (20) via a second line (32). A shut-off device (36; 52) of the differential pressure sensor system (12) is arranged in the second line (32) which is switchable between an open position (P1) in which it opens the second line (32) such that a pressure prevailing in the aircraft environment (20) acts on the second port (28) of the differential pressure sensor (22), and a shut-off position (P2) in which it closes the second line (32) such that the second port (28) of the differential pressure sensor (22) is shut off from the pressure prevailing in the aircraft environment (20).


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    Titel :

    DIFFERENTIAL PRESSURE SENSOR SYSTEM, AIRCRAFT EQUIPPED WITH A DIFFERENTIAL PRESSURE SENSOR SYSTEM AND METHOD FOR OPERATING A DIFFERENTIAL PRESSURE SENSOR SYSTEM


    Weitere Titelangaben:

    DIFFERENZDRUCKSENSORSYSTEM, MIT EINEM DIFFERENZDRUCKSENSORSYSTEM AUSGESTATTETES FLUGZEUG UND VERFAHREN ZUM BETRIEB EINES DIFFERENZDRUCKSENSORSYSTEMS
    SYSTÈME DE CAPTEUR DE PRESSION DIFFÉRENTIELLE, AÉRONEF ÉQUIPÉ D'UN SYSTÈME DE CAPTEUR DE PRESSION DIFFÉRENTIELLE ET PROCÉDÉ POUR FAIRE FONCTIONNER UN SYSTÈME DE CAPTEUR DE PRESSION DIFFÉRENTIELLE


    Beteiligte:
    WAIGL ILJA (Autor:in) / MAIL MATIAS (Autor:in) / KNIJNENBURG THORSTEN (Autor:in)

    Erscheinungsdatum :

    2018-11-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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





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