A method is provided for component management. During this method, a first output signal is received from a first aircraft system at a component management system. The first aircraft system includes a first engine and a first component installed in the first engine. The first output signal communicates identification data for the first engine and a first operating parameter for the first engine. A first component parameter for the first component is determined based on the identification data for the first engine and the first operating parameter for the first engine. A record for the first component is updated in the component management system using the first component parameter for the first component.


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    Title :

    MANAGEMENT OF AIRCRAFT SYSTEM COMPONENTS ACROSS DIFFERENT AIRCRAFT ENGINES


    Contributors:
    BRILLON LOUIS (author) / SHI SONGYUE (author)

    Publication date :

    2025-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    MANAGEMENT OF AIRCRAFT SYSTEM COMPONENTS ACROSS DIFFERENT AIRCRAFT ENGINES

    VARENNES LOUIS BRILLON / SHI SONGYUE | European Patent Office | 2025

    Free access



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