@inproceedings{c2e16063660c415f800aa401ee0b7d4a,
title = "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.",
keywords = "Load simulation, Mathematical model, Nose landing gear steering, Position servo system, Proportional relief valve",
author = "Zhang, \{Lin Hai\} and Qi, \{Xiao Ye\} and Ma, \{Jun Gong\} and Yang, \{Rong Rong\}",
note = "Publisher Copyright: {\textcopyright} (2014) Trans Tech Publications, Switzerland.; 2014 International Conference on Manufacturing Technology and Electronics Applications, ICMTEA 2014 ; Conference date: 08-11-2014 Through 09-11-2014",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.687-691.701",
language = "英语",
series = "Applied Mechanics and Materials",
publisher = "Trans Tech Publications Ltd",
pages = "701--705",
editor = "Zhang Lin and Hongying Hu and Yajun Zhang and Jianguo Qiao and Jiamin Xu",
booktitle = "Manufacturing Technology, Electronics, Computer and Information Technology Applications",
address = "瑞士",
}