An aircraft interface device (12) receives aircraft system data over an aircraft data bus structure (26) and remote data received via a wireless transceiver. The remote data originates from a computing device that is remote from the aircraft and/or aircraft system devices installed on the aircraft. The aircraft interface (12) device executes a conditional algorithm that includes a plurality of conditional expressions (40; 48A-48F) that are logically organized to define a trigger (42; 50) that initiates a triggered action (44; 52A-52C). The plurality of conditional expressions (40; 48A-48F) include a first conditional expression based upon the aircraft system data and a second conditional expression based upon the remote data. The aircraft interface device (12) executes the triggered action (44; 52A-52C) responsive to determining that the trigger (42; 50) is satisfied. The triggered action (44; 52A-52C) includes at least one of transmitting an alert, transmitting a report, and storing a report.


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    Titel :

    AIRCRAFT CONDITION MONITORING SYSTEM


    Weitere Titelangaben:

    FLUGZEUGZUSTANDSÜBERWACHUNGSSYSTEM
    SYSTÈME DE SURVEILLANCE DE L'ÉTAT D'UN AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    23.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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