Reliability Analysis of Aircraft Hydraulic Control System based on GO Methodology
Lina Zhang, Yanjun Li, Jian Zhang
Available Online March 2016.
- 10.2991/icmmct-16.2016.319How to use a DOI?
- Aircraft Hydraulic System; Reliability Analysis; GO Methodology
Aircraft hydraulic system is an important part of an aircraft, its reliability is of great significance to the aircraft flight safety. This paper puts forward an aircraft reliability analysis method of hydraulic control system based on the GO methodology, which is based on the thorough research of GO methodology and aircraft hydraulic control system. Firstly, simplify the aircraft hydraulic control system principle diagram and establish the GO diagram. Then, establish the GO diagram according to the reliability of each component. Finally, calculate the reliability of the hydraulic control system based on the principle of GO diagram and operation rules and improve the reference for the design of aircraft hydraulic system.
- © 2016, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Lina Zhang AU - Yanjun Li AU - Jian Zhang PY - 2016/03 DA - 2016/03 TI - Reliability Analysis of Aircraft Hydraulic Control System based on GO Methodology BT - Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology PB - Atlantis Press SP - 1601 EP - 1605 SN - 2352-5401 UR - https://doi.org/10.2991/icmmct-16.2016.319 DO - 10.2991/icmmct-16.2016.319 ID - Zhang2016/03 ER -