A method for pressurizing and depressurizing 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 pressurization level of a shock absorber. As such, the shock absorber may be pressurized to the correct level without applying an iterative approach, greatly reducing initialization time.
LANDING GEAR STORAGE AND QUICK SERVICING SOLUTION
2017-12-07
Patent
Electronic Resource
English
SAE Technical Papers | 2013
SAE Technical Papers | 2018