Open Access
Issue |
MATEC Web Conf.
Volume 114, 2017
2017 International Conference on Mechanical, Material and Aerospace Engineering (2MAE 2017)
|
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Article Number | 03016 | |
Number of page(s) | 8 | |
Section | Chapter 3: Aerospace | |
DOI | https://doi.org/10.1051/matecconf/201711403016 | |
Published online | 10 July 2017 |
- Aircraft design manual general editorial board. Aircraft design manual 14: Takeoff and landing system design[M]. Beijing: Aviation Industry Press, 2002. [Google Scholar]
- Boitsov. Reliability of aircraft landing gear. Zhen Guo, Peifan Guo, translation. Beijing: national defence industry press, 2002. [Google Scholar]
- Civil Aviation Administration of China 2001Part 2-airworthiness standards: transport category airplane (Beijing) pp 181-183. [Google Scholar]
- Yao Xiao, Yifei Tang, Hong Cao. R&D of high pressure pneumatic ELGE system[J]. Hydraulics Pneumatics & seals, 2015, 06: 61-63. [Google Scholar]
- Cunfang Zhang, Yongsheng Feng. Research on landing gear emergency Extending System[J]. Civil Aircraft Design and Research, 2010(1): 19-21. [Google Scholar]
- Beaver aerospace & defence. Electromechanical actuator(EMAS)[EB/OL]. 2013-5-23. http://www.beaver-online.com/64.html. [Google Scholar]
- Kai Chang, Shengjun Li. Application and development of more electrical technology in landing gear system[J]. Aeronautical Science & Technology, 2014, 25(07): 01-05. [Google Scholar]
- Lin Li. Research for dual redundancy electromechanical actuation system of UAV landing gear[M]. NUAA, nanjing, 2013. [Google Scholar]
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