The present invention relates to a method for pressurising and depressurising a shock absorber of an aircraft. More specifically, it relates to a method in which an aircraft weight and ambient temperature are used to calculate a required pressurisation level of a shock absorber. As such, the shock absorber may be pressurised to the correct level without applying an iterative approach, greatly reducing initialisation time.
LANDING GEAR STORAGE AND QUICK SERVICING SOLUTION
FAHRWERKAUFBEWAHRUNGS- UND -SCHNELLWARTUNGSLÖSUNG
SOLUTION DE STOCKAGE ET D'ENTRETIEN RAPIDE D'UN TRAIN D'ATTERRISSAGE
2021-05-19
Patent
Electronic Resource
English
SAE Technical Papers | 2013
SAE Technical Papers | 2018