A cabin pressure sensor system (100) for an aircraft including a plurality of air pressure sensors (104) positioned within an aircraft environment, an indication device (106), a central processing unit (CPU) (102) electrically coupled to the plurality of air pressure sensors (104) and the indication device (106), being configured to receive air pressure measurements from each of the first air pressure sensor and the second air pressure sensor, defining received air pressure measurements, identify received air pressure measurements that are below the minimum cabin air pressure limit, defining an anomalous cabin air pressure measurement, and operate the indication device (106) responsive to identifying an anomalous cabin air pressure measurement. The system (100) further includes a power supply device (108) electrically coupled to the CPU, the sensor, and the indication device (106).


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    Titel :

    CABIN PRESSURE SENSOR (CPS) SYSTEM FOR PRESSURIZED-CABIN AIRCRAFT AND ASSOCIATED METHODS


    Weitere Titelangaben:

    KABINENDRUCKSENSOR (CPS)-SYSTEM FÜR DRUCKKABINE EINES FLUGZEUGS UND ZUGEHÖRIGE VERFAHREN
    SYSTÈME DE CAPTEURS DE PRESSION DE CABINE (CPS) POUR AÉRONEF À CABINE PRESSURISÉE ET PROCÉDÉS ASSOCIÉS


    Beteiligte:
    TELLES ANGEL (Autor:in) / ROOF NICHOLAS (Autor:in) / OAKLEY CHRISTOPHER (Autor:in) / HEICK EDWARD (Autor:in)

    Erscheinungsdatum :

    30.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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