Reliability Analysis of Aircraft Hydraulic Control System based on GO Methodology

DOI

10.2991/icmmct-16.2016.319How to use a DOI?

Keywords

Aircraft Hydraulic System; Reliability Analysis; GO Methodology

Abstract

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.

Copyright

© 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/).

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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  -