Study on the Reliability Evaluation of Typical Light Electric Aircraft

DOI

10.2991/icmit-16.2016.138How to use a DOI?

Keywords

Electric light aircraft, Failure mode and effects analysis, Probability distribution function, Key components, Criticality, Fault Tree

Abstract

The reliability level of electric light aircraft is the core index of judging the safety level of its flight. In this paper, the theory and method of reliability determination of Rui-Xiang electric aircraft are studied from the perspective of intrinsic safety. On the basis of Extensive research and data analysis, it studies the reliability to determine the basic method and the basic structure and composition, discusses the key components and the critical degree of determination and calculation method. Then, using FME(C)A to identify key components of the aircraft landing gear systems, determine the harm degree of key components and calculate the critical degree of key components. The reliability level of Rui-Xiang aircraft are studied with comprehensively analysis. The results can provide theoretical guidance of reliability analysis and evaluation of the electric light aircraft.

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  - Xingbai Zhang
AU  - Qingmin Si
AU  - Lei Tian
AU  - Gongxin Yu
AU  - Xueying Jiang
PY  - 2016/04
DA  - 2016/04
TI  - Study on the Reliability Evaluation of Typical Light Electric Aircraft
BT  - Proceedings of the 2016 3rd International Conference on Mechatronics and Information Technology
PB  - Atlantis Press
SP  - 764
EP  - 767
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmit-16.2016.138
DO  - 10.2991/icmit-16.2016.138
ID  - Zhang2016/04
ER  -