A method and an apparatus to monitor components of an aircraft landing system are disclosed herein. The method includes determining a first temperature of a wheel of an aircraft via a first temperature sensor, and determining a second temperature of a brake assembly operatively coupled to the wheel via a second temperature sensor. The method further includes estimating a peak temperature of a fuse plug disposed on the wheel based on the first temperature and the second temperature.


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    Title :

    Method to monitor components of an aircraft landing system


    Additional title:

    Verfahren zur Überwachung von Komponenten eines Flugzeuglandesystems
    Procédé pour surveiller des composants de système d'atterrissage d'un avion


    Contributors:

    Publication date :

    2020-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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