Special Topic of Electric Aircraft

Spoiler system reliability of certain electric aircraft based on Matrix-GO method

  • LI Jingkui ,
  • WANG Ying ,
  • WANG Bomin
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  • Civil Aviation College, Shenyang Aerospace University, Shenyang 110136, China

Received date: 2020-03-09

  Revised date: 2020-06-19

  Online published: 2020-07-06

Supported by

Key Projects of Liaoning Provincial Department of Education(JYT19003);Natural Science Foundation of Liaoning Province (20180550279);Shenyang Science and Technology Plan Project(18-400-2-07)

Abstract

The spoiler redundancy system improves the reliability of new energy electric aircraft. A reliability model of electric airplane spoiler systems is established by the GO method, a SIMULINK simulation interface designed, and a new operation module provided for operator 11. To effectively reduce the workload of the traditional GO method in redundant system modeling, we design a kind of moment operator for the spoiler redundant system, with the results verified by fault tree analysis. The results show that the method proposed in this paper is feasible, therefore providing a new idea for reliability analysis of the spoiler system of new energy electric aircraft.

Cite this article

LI Jingkui , WANG Ying , WANG Bomin . Spoiler system reliability of certain electric aircraft based on Matrix-GO method[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021 , 42(3) : 623945 -623945 . DOI: 10.7527/S1000-6893.2020.23945

References

[1] 黄俊,杨凤田.新能源电动飞机发展与挑战[J].航空学报,2016,37(1):57-68. HUANG J,YANG F T.Development and challenges of electirc aircraft with new energies[J].Acta Aeronautica et Astronautica Sinica,2016,37(1):57-68(in Chinese).
[2] TAKAHASHI K,FUJIMOTO H,HORI Y.Modeling of propeller electric airplane and thrust control using advantage of electric motor[C]//IEEE International Workshop on Advanced Motion Control.Piscataway:IEEE Press,2014:482-487.
[3] STEINER H,VRATNY P C,GOLOGAN C,et al.Optim-um number of engines for transport aircraft employing electrically powered distributed propulsion[J].CEAS Aeronautical Journal,2015,5(2):157-170.
[4] 丰世林.基于AMESim的某型运输机地面扰流板内漏故障研究[J].机床与液压,2017,45(22):190-193,198. FENG S L.Research on the internal leakage fault of the ground spoiler of a certain transporter based on AMESim[J]. Machine Tool & Hydraulics, 2017, 45(22):190-193,198(in Chinese).
[5] 郁明辉,李鹏,刘肖肖.民航客机扰流板模拟器刚度仿真与试验[J].航天控制,2019,37(3):31-35. YU M H,LI P,LIU X X.Stiffness simulation and experiment of spoiler simulator for civil airliner[J].Aerospace Control, 2019,37(3):31-35(in Chinese).
[6] 沈祖培,高佳.GO法原理和改进的定量分析方法[J].清华大学学报(自然科学版),1999(6):16-20. SHEN Z P,GAO J.Principle of GO method and improved quantitative analysis method[J].Journal of Tsinghua University (Science and Technology), 1999(6):16-20(in Chinese).
[7] 沈祖培,黄祥瑞.GO法原理及应用:一种系统可靠性分析方法[M].北京:清华大学出版社,2004. SHEN Z P,HUANG X R.GO method principle and application:An analysis method of system reliability[M]. Beijing:Tsinghua University Press, 2004(in Chinese).
[8] YI X J,DHILLON B S,DONG H P,et al.Quantitative reliability analysis of repairable systems with closed-loop feedback based on GO methodology[J].Journal of the Brazilian Society of Mechanical Sciences and Engineering,2017,39(5):1845-4858.
[9] REN Y,FAN D M,WANG Z L,et al.System dynamic behavior modeling based on extended GO methodology[J].IEEE Access,2018,6:22513-22523.
[10] 马骏,段富海,王海朋.基于GO法的某型飞机液压系统可靠性研究[J].大连理工大学学报,2019,59(5):492-500. MA J,DUAN F H, WANG H P.Research on the reliability of a certain aircraft hydraulic system based on GO method[J].Journal of Dalian University of Technology,2019,59(5):492-500(in Chinese).
[11] 王海朋,段富海,江秀红.基于模糊GO法的惯性导航系统可靠性研究[J].大连理工大学学报,2018,58(3):285-292. WANG H P,DUAN F H,JIANG X H.Reliability research of inertial navigation system based on fuzzy GO method[J].Journal of Dalian University of Technology, 2018,58(3):285-292(in Chinese).
[12] 黄涛,蔡琦,赵新文,等.SIMULINK仿真技术在压水堆净化系统可靠性GO法分析中的应用[J].核动力工程,2010,31(1):88-91. HUANG T, CAI Q, ZHAO X W, et al.Application of SIMULINK simulation technology in GO method analysis of PWR purification system reliability[J].Nuclear Power Engineering,2010,31(1):88-91(in Chinese).
[13] 江秀红,段富海,金霞,等.状态概率矩阵及其在GO法中应用[J].大连理工大学学报,2014,54(2):176-181. JIANG X H, DUAN F H, JIN X, et al. State probability matrix and its application in GO method[J].Journal of Dalian University of Technology,2014, 54(2):176-181(in Chinese).
[14] 张丽娜,李艳军,张建.基于模糊GO法的飞机备件支援系统可靠性分析[J].科学技术与工程,2017,17(4):105-109,116. ZHANG L N,LI Y J,ZHANG J.Reliability analysis of aircraft spare parts support system based on fuzzy GO method[J]. Science Technology and Engineering, 2017, 17(4):105-109,116(in Chinese).
[15] 李玉峰,宁昭义.电动飞机电推进系统可靠性建模与仿真[J].计算机仿真,2019,36(1):51-56. LI Y F, NING Z Y.Reliability modeling and simulation of electric propulsion system for electric aircraft[J].Computer Simulation,2019,36(1):51-56(in Chinese).
[16] 郑坤. 基于GO法的复杂配电系统可靠性研究[D].西安:西安理工大学,2007. ZHENG K.Research on reliability of complex power distribution system based on GO method[D]. Xi'an:Xi'an University of Technology, 2007(in Chinese).
[17] 刘宇阳,龚庆武,梁志远.基于改进GO法的继电保护系统可靠性分析[J].电力科学与技术学报, 2016,31(4):129-135. LIU Y Y,GONG Q W,LIANG Z Y.Reliability analysis of relay protection system based on improved GO method[J].Journal of Electric Power Science and Technology, 2016,31(4):129-135(in Chinese).
[18] 田录林,刘沛盛.改进贝叶斯网络GO法在高压直流输电系统的可靠性分析[J].高压电器,2017,53(7):53-59,66. TIAN L L,LIU P S.Reliability analysis of improved bayesian network GO method in HVDC transmission system[J].High Voltage Apparatus, 2017,53(7):53-59,66(in Chinese).
[19] 闫锋,尚永锋,付继龙.基于故障树-蒙特卡罗模拟的航空发动机控制系统适航审定安全性分析方法[J].科学技术与工程,2019,19(29):363-370. YAN F,SHANG Y F,FU J L.Safety analysis method for airworthiness certification of aero-engine control system based on fault tree-Monte Carlo simulation[J].Science Technology and Engineering,2019,19(29):363-370(in Chinese).
[20] 宋俊花,魏欧.基于线性时间算法的故障树模块扩展分解方法[J].计算机科学,2019,46(1):226-231. SONG J H,WEI O.A linear time algorithm based fault tree module expansion method[J].Computer Science,2019,46(1):226-231(in Chinese).
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