Methods and Apparatus to monitor components of an aircraft landing system are disclosed herein. An example method includes determining an initial temperature of at least one of a wheel or a fuse plug based on a temperature value to be provided by a first temperature sensor; estimating a temperature of a brake assembly based on a temperature value provided by a second temperature sensor; after determining the initial temperature, estimating a subsequent temperature of the at least one of the wheel or the fuse plug; and determining if the subsequent temperature is a peak temperature.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Methods and apparatus to monitor components of an aircraft landing system


    Beteiligte:

    Erscheinungsdatum :

    2019-07-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01K MEASURING TEMPERATURE , Messen der Temperatur / 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



    METHODS AND APPARATUS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM

    MILLER TRENT DARYL | Europäisches Patentamt | 2016

    Freier Zugriff

    METHODS AND APPARATUS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM

    MILLER TRENT DARYL | Europäisches Patentamt | 2016

    Freier Zugriff

    Methods to monitor components of an aircraft landing system

    MARTIN CASANDRA JOLENE | Europäisches Patentamt | 2016

    Freier Zugriff

    METHODS TO MONITOR COMPONENTS OF AN AIRCRAFT LANDING SYSTEM

    MARTIN CASANDRA JOLENE | Europäisches Patentamt | 2018

    Freier Zugriff

    Methods to monitor components of an aircraft landing system

    MARTIN CASANDRA JOLENE | Europäisches Patentamt | 2017

    Freier Zugriff