A method for monitoring configuration of an aircraft engine including a plurality of pieces of equipment each having a radio identification device, associated with a reference configuration including a set of reference identification data per piece of equipment, including automatically reading each radio identification device to obtain a configuration including at least one set of identification data read per piece of equipment; for each piece of equipment for which the set of identification data read is different from the set of reference identification data: if the set of identification data read corresponds to a set of replacement identification data associated with an operation for replacing the piece of equipment, replacing the set of reference identification data by the set of identification data read; otherwise, generating an alert.


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    Title :

    PROCÉDÉ DE SUIVI DE LA CONFIGURATION D'UN MOTEUR D'AÉRONEF ET SYSTÈME ASSOCIÉ


    Additional title:

    METHOD FOR MONITORING THE CONFIGURATION OF AN AIRCRAFT ENGINE, AND ASSOCIATED SYSTEM
    VERFAHREN ZUR ÜBERWACHUNG DER KONFIGURATION EINES FLUGZEUGMOTORS UND ZUGEHÖRIGES SYSTEM



    Publication date :

    2024-09-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G06Q Datenverarbeitungssysteme oder -verfahren, besonders angepasst an verwaltungstechnische, geschäftliche, finanzielle oder betriebswirtschaftliche Zwecke, sowie an geschäftsbezogene Überwachungs- oder Voraussagezwecke , DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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