An apparatus and method 300 for determining a temperature characteristic at a first location on a wheel 104 or a brake assembly 200 of an aircraft landing gear 102. The apparatus comprises a processor configures to determine the temperature characteristic at the first location using relationship information based on a first temperature at a second location 104 of the wheel or the brake assembly of the landing gear, the relationship information representing a relationship between the temperature characteristic at the first location and the first temperature, allowing the first temperature to be estimated. Also disclosed is a method to determine the relationship information between the first and second locations and an apparatus for determining a plurality of temperature parameters at a first location. The first location may be a fuse plug 220a of a tyre 204 of the landing gear and the second location may be a brake disk 202 of a brake assembly of the landing gear.


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    Title :

    Landing gear temperature characteristic


    Contributors:

    Publication date :

    2019-09-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / G01K MEASURING TEMPERATURE , Messen der Temperatur / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge



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