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All-Electric Aircraft Nose Wheel Steering System with Two Worm Gears

Zhang M ing Li Chuang Wu Xin Zhu Yin

南京航空航天大学学报(英文版)2018,Vol.35Issue(1):170-180,11.
南京航空航天大学学报(英文版)2018,Vol.35Issue(1):170-180,11.

All-Electric Aircraft Nose Wheel Steering System with Two Worm Gears

All-Electric Aircraft Nose Wheel Steering System with Two Worm Gears

Zhang M ing 1Li Chuang 2Wu Xin 3Zhu Yin3

作者信息

  • 1. Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics & Astronautics,Nanjing 210016,P.R.China
  • 2. Shanghai Aircraft Design and Research Institute,Shanghai 201210,P.R.China
  • 3. Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration, Nanjing 211106,P.R.China
  • 折叠

摘要

关键词

mechanotronics design/nose wheel steering system/all-electric/aircraft design/landing gear

Key words

mechanotronics design/nose wheel steering system/all-electric/aircraft design/landing gear

分类

航空航天

引用本文复制引用

Zhang M ing,Li Chuang,Wu Xin,Zhu Yin..All-Electric Aircraft Nose Wheel Steering System with Two Worm Gears[J].南京航空航天大学学报(英文版),2018,35(1):170-180,11.

基金项目

This work was supported partly by the Aeronautical Science Foundation of China(No.20142852025). (No.20142852025)

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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