The Load Simulation Research of Nose Landing Gear Steering

Abstract:

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.

• Periodical: Applied Mechanics and Materials (Volumes 687-691)
• Pages: 701-705
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.687-691.701
• Online since: November 2014
• Authors: Lin Hai Zhang*, Xiao Ye Qi, Jun Gong Ma, Rong Rong Yang
• Keywords: Load Simulation, Mathematical Models, Nose Landing Gear Steering, Position Servo System, Proportional Relief Valve

References

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DOI: 10.1109/indin.2012.6301057