Civil aircraft landing gear brake system development and evaluation using model based system engineering

2017 ◽  
Author(s):  
Xiaohang Hai ◽  
Shaojie Zhang ◽  
Xiaodong Xu
Keyword(s):  
System Development ◽  
System Engineering ◽  
Landing Gear ◽  
Brake System ◽  
Model Based ◽  
Aircraft Landing ◽  
Aircraft Landing Gear ◽  
Civil Aircraft

The Load Simulation Research of Nose Landing Gear Steering

2014 ◽  
Vol 687-691 ◽  
pp. 701-705
Author(s):  
Lin Hai Zhang ◽  
Xiao Ye Qi ◽  
Jun Gong Ma ◽  
Rong Rong Yang
Keyword(s):  
Landing Gear ◽  
Durability Test ◽  
Simulation Research ◽  
Aircraft Landing ◽  
Aircraft Landing Gear ◽  
Civil Aircraft ◽  
Vital Component ◽  
Load Simulation ◽  
The Mathematical Model ◽  
Rack Mechanism

The nose landing gear is a vital component of an aircraft,which has an important impact on the safety of the aircraft.This paper studies the system of nose landing gear steering on the basis of the gear and rack mechanism durability test of a certain type of civil aircraft landing gear steering. Furthermore,it puts forward a method of passive loading,which can simulate the friction when the nose landing gear reciprocating turning,and establishes the mathematical model. The simulation results show that the simulator can meet the requirements of load,and laid a theoretical foundation for the subsequent actual work.

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