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.
Method to monitor components of an aircraft landing system
Verfahren zur Überwachung von Komponenten eines Flugzeuglandesystems
Procédé pour surveiller des composants de système d'atterrissage d'un avion
2020-11-04
Patent
Electronic Resource
English
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