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.
Methods to monitor components of an aircraft landing system
Verfahren zur Überwachung der Komponenten eines Flugzeuglandesystems
Procédés pour surveiller des composants de système d'atterrissage d'un avion
2017-06-14
Patent
Electronic Resource
English
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