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.


    Access

    Download


    Export, share and cite



    Title :

    Methods to monitor components of an aircraft landing system


    Contributors:

    Publication date :

    2016-01-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / G01K MEASURING TEMPERATURE , Messen der Temperatur



    METHODS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM

    MARTIN CASANDRA JOLENE | European Patent Office | 2018

    Free access

    Methods to monitor components of an aircraft landing system

    MARTIN CASANDRA JOLENE | European Patent Office | 2017

    Free access

    METHODS AND APPARATUS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM

    MILLER TRENT DARYL | European Patent Office | 2016

    Free access

    METHODS AND APPARATUS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM

    MILLER TRENT DARYL | European Patent Office | 2016

    Free access

    Methods and apparatus to monitor components of an aircraft landing system

    MILLER TRENT DARYL | European Patent Office | 2019

    Free access