Health Assessment of Landing Gear Retraction/Extension Hydraulic System Based on Improved Risk Coefficient and FCE Model

被引:6
作者
Duan, Shixuan [1 ]
Li, Yanjun [1 ]
Cao, Yuyuan [1 ]
Wang, Xingye [1 ]
Li, Xudong [1 ]
Zhao, Zejian [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Civil Aviat, Nanjing 210016, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2022年 / 12卷 / 11期
关键词
health assessment; landing gear retraction; extension hydraulic system; improved risk coefficient; fuzzy comprehensive evaluation; fault simulation; maintenance manual; AIRCRAFT;
D O I
10.3390/app12115409
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Featured Application A more objective assessment technique is proposed to lessen the reliance on expert opinion in the health evaluation procedure of the landing gear hydraulic retraction/extension system. The health of the landing gear retraction/extension(R/E) hydraulic system may be assessed using fuzzy comprehensive evaluation (FCE), however the traditional FCE method depends solely on human assessment by specialists, which is excessively subjective. To address the issue of excessive human subjective variables in the assessment, an improved FCE model based on enhanced risk coefficient is provided, which includes four consideration indexes: failure probability, failure severity, failure detection difficulty, and failure repair difficulty. To reduce subjective human judgment errors entirely due to expert experience, the improved FCE takes into account the likelihood of failure using a statistical method, the severity of failure using a fault simulation analysis based on the LMS Imagine.Lab AMESim simulation platform, and the difficulty of fault detection and repair using the aircraft manufacturer's professional maintenance information. As part of the evaluation model, the range of health assessment values and accompanying treatment methods are included, making it easier to implement on a daily basis in aircraft maintenance. As a final step, the simulation is evaluated, and the simulated faults are calculated.
引用
收藏
页数:23
相关论文
共 42 条
[1]  
[Anonymous], 2012, THESIS CRANFIELD U L
[2]  
[Anonymous], P AIAA GUID NAV CONT
[3]  
[Anonymous], 2010, B737600700800900
[4]   RISK ANALYSIS APPROACH TO TRANSPORT AIRCRAFT TECHNOLOGY-ASSESSMENT [J].
BATSON, RG ;
LOVE, RM .
JOURNAL OF AIRCRAFT, 1988, 25 (02) :99-105
[5]   Structural health monitoring-based methodologies for managing uncertainty in aircraft structural life assessment [J].
Bond, Ray ;
Underwood, Sara ;
Adams, Douglas E. ;
Cummins, Joshua J. .
STRUCTURAL HEALTH MONITORING-AN INTERNATIONAL JOURNAL, 2014, 13 (06) :621-628
[6]   Data-Driven Health Assessment in Flight Control System [J].
Chen, Jie ;
Zhao, Yuyang ;
Wu, Chentao ;
Xu, Qingshan .
APPLIED SCIENCES-BASEL, 2020, 10 (23) :1-14
[7]   Health Monitoring of Landing Gear Retraction/Extension System Based on Optimized Fuzzy C-Means Algorithm [J].
Chen, Jie ;
Chen, Senyao ;
Liu, Zhenbao ;
Luo, Caikun ;
Jing, Zhengdong ;
Xu, Qingshan .
IEEE ACCESS, 2020, 8 :219611-219621
[8]   Risk assessment of corroded casing based on analytic hierarchy process and fuzzy comprehensive evaluation [J].
Chen, Sheng-Shan ;
Wang, Han-Xiang ;
Jiang, Hao ;
Liu, Ya-Nan ;
Liu, Yan-Xin ;
Lv, Xiao-Xiao .
PETROLEUM SCIENCE, 2021, 18 (02) :591-602
[9]  
Chen Ying-wu, 2006, Journal of National University of Defense Technology, V28, P126
[10]   Wear failure analysis of suction valve for high pressure and large flow water hydraulic plunger pump [J].
Dong, Jie ;
Deng, Yipan ;
Cao, Wenbin ;
Wang, Zhongkai ;
Ma, Wensheng ;
Wu, Defa ;
Ji, Hong ;
Liu, Yinshui .
ENGINEERING FAILURE ANALYSIS, 2022, 134