Methods to monitor components of an aircraft landing system are disclosed herein. An example method includes determining a brake assembly temperature and determining a wheel temperature. The example method also includes retrieving an estimated increase in the wheel temperature from a data structure based on the wheel temperature and the brake assembly temperature. The example method further includes determining a maximum wheel temperature based on the wheel temperature and the estimated increase in the wheel temperature.

    Linvention propose des procédés pour surveiller des composants dun système datterrissage davion. Un exemple dun procédé comprend la détermination de la température dun ensemble de freinage et la détermination dune température de roue. Un exemple de procédé comprend également la récupération dune augmentation évaluée de la température de roue à partir dune structure de données basée sur la température de roue et la température dun ensemble de freinage. Lexemple dun procédé comprend en outre la détermination dune température de roue maximale basée sur la température de roue et laugmentation évaluée de la température de roue.


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    Title :

    METHODS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM


    Additional title:

    PROCEDES POUR SURVEILLER DES COMPOSANTS D'UN SYSTEME D'ATTERRISSAGE D'AVION


    Contributors:

    Publication date :

    2018-03-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60C VEHICLE TYRES , Fahrzeugreifen / B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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