期刊文献+

服役飞机结构件腐蚀失效故障树分析及改进 被引量:9

Fault tree analysis of corrosion failure for aircraft structures and improvements
下载PDF
导出
摘要 对某出口用飞机铝合金结构件在热带海洋大气环境条件下服役时所发生的腐蚀失效问题,提出了采用故障树分析方法对引起飞机结构件腐蚀失效的各因素进行系统分析和探讨.根据结构件腐蚀失效过程及机理的分析,确定导致结构件腐蚀失效的各个因素,建立以结构件腐蚀失效为顶事件的故障树,通过布尔代数运算得到故障树的各阶最小割集.计算故障树顶事件的发生概率,并对底事件的概率重要度、相对概率重要度进行分析排序,找出引起铝合金结构件发生腐蚀失效的主要因素.分析结果表明飞机服役环境、阳极氧化工艺和选材是导致结构件腐蚀失效的主要因素.针对这些主要因素,提出了相应的改进防护措施. To analyze corrosion failure of aluminum alloy structures on export airplane used in marine environment,the fault tree analysis was proposed to analyze the erosion factors of aircraft structures.Through investigating and analyzing on failure processes and failure mechanism of structural components of aluminum alloy on airplane,factors which brought on erosion of structural parts were found.Fault tree of corrosion failure was set up and the minimal cut-sets were obtained by Boolean operation,and the top-event occurrence rate was calculated.The probability importance and relative probability importance of bottom events were analyzed and arranged,and then the important bottom events which caused corrosion of aluminum alloy structures were found.Results show that the main factors which caused corrosion of aircraft structures are ocean environment,anodic oxidation and select material.Some improvements with respect to the main factors had been proposed.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2010年第3期299-302,共4页 Journal of Beijing University of Aeronautics and Astronautics
关键词 飞机结构件 腐蚀失效 故障树分析 最小割集 概率重要度 aircraft structure corrosion failure fault tree analysis minimal cut-set probability importance
  • 相关文献

参考文献8

  • 1黄领才,谷岸,刘慧丛,姜同敏.海洋环境下服役飞机铝合金零件腐蚀失效分析[J].北京航空航天大学学报,2008,34(10):1217-1221. 被引量:18
  • 2Robinson M J. The role of wedging stresses in the exfoliation corrosion of high strength aluminium alloys[ J ]. Corrosion Science, 1983,23(8) :887 -899.
  • 3韩德盛,李荻.LY12铝合金在海洋大气环境下加速腐蚀试验和外场暴露试验的相关性[J].腐蚀与防护,2008,29(3):119-120. 被引量:13
  • 4Contini S,Cojazzi G G M, Renda G. On the use of non-coherent fault trees in safety and security studies [ J]. Reliability Engineering and System Safety,2008,93:1886 - 1895.
  • 5Dan M Shalev, Joseph Tiran. Condition-based fault tree analysis [J ]. Reliability Engineering and System Safety, 2007, 92: 1231 - 1241.
  • 6Dong Yuhua, Yu Datao. Estimation of failure probability of oil and gas transmission pipelines by fuzzy fault tree analysis [ J ]. Journal of Loss Prevention in the Process Industries,2005,18:83 -88.
  • 7Demichela M,Piccinini N,Ciarambino 1. On the numerical solution of fault trees[ J ]. Reliability Engineering and System Safety, 2003,82 : 141 - 147.
  • 8Rajasekaran B, Raman S G S, Krishnab L R, et al. Influence of microarc oxidation and hard anodizing on plain fatigue and fret- ting fatigue behaviour of AI Mg Si alloy[ J]. Surface and Coatings Technology ,2008,202 ( 8 ) : 1462 - 1469.

二级参考文献15

  • 1陈群志,崔常京,孙祚东,王逾涯,席慧智.LY12CZ铝合金腐蚀损伤的概率分布及其变化规律[J].装备环境工程,2005,2(3):1-6. 被引量:24
  • 2鲁效梅.铝合金挤压型材剥层腐蚀研究[J].西飞科技,1995(2):12-16. 被引量:4
  • 3李获,左尚志,郭宝兰.LY12铝合金剥蚀行为的研究[J].中国腐蚀与防护学报,1995,15(3):203-209. 被引量:36
  • 4Rhodes D, Radon J C. Fracture analysis of exfoliation in an aluminium alloy [J].Engineering Fracture Mechanics, 1978, 10 (4) :843 - 853
  • 5Robinson M J. The role of wedging stresses in the exfoliation corrosion of high strength aluminium alloys[ J]. Corrosion Science, 1983, 23(8) :887 -899
  • 6Ketchem S J, Jankowsky E J. Hhipboard exposure test of aluminum alloys[R]. AFWAL-TR-81-4019,1980
  • 7Posada M, Murr L E, Niou C S, et al. Exfoliation and related microstructures in 2024 aluminum body skins on aging aircraft [ J]. Materials Characterization, 1997, 38 (4/5) :259 - 272
  • 8Conde A, Damborenea J. Electrochemlcal modellng of exfoliation corrosion behavior of 8090 alloy[J]. Electrochimica Acta, 1998, 43(8) :849 -860
  • 9Ketcham S J. Accelerated laboratory corrosion test for materials and finishes used in naval aircraft[R]. ADA048059, 1977
  • 10Reboul M C, Dubost B, Lashermes M. The stress corrosion susceptibility of aluminium alloy 7020 welded sheets[J]. Corrosion Science, 1985, 25 ( 11 ) :999 - 1018

共引文献29

同被引文献59

  • 1杨维垣.空间机构分类及可靠性研究[J].航天器工程,1994,3(1):31-39. 被引量:8
  • 2易云兵,姚安林.埋地输气管道腐蚀失效故障树分析[J].天然气与石油,2005,23(5):13-16. 被引量:7
  • 3陈群志,崔常京,王逾涯,张蕾.典型机场地面腐蚀环境数据库研究[J].装备环境工程,2006,3(3):47-49. 被引量:12
  • 4谢云杰,姚安林,钱浩.海底管道系统失效故障树的建立及定性分析[J].中国海上油气(工程),2006,18(3):213-216. 被引量:9
  • 5任必年.公路桥梁腐蚀与防护[M].北京:人民交通出版社,2002.
  • 6Russo S,Sharp P K,Mills T B,et al.The influence of the environment and corrosion on the structural integrity of aircraft materials [J].Fatigue and Fracture of Engineering Materials and Structures.2009,32(6):464-472.
  • 7Pitting corrosion of cast metallurgy aluminum-beryllium alloys in sulfuric acid solutions [J].Corrosion,2008,64(6):517-531.
  • 8Burleigh T D,Ludwiczak E,Petri R A.Intergranular corrosion of an aluminum-magnesium-silicon-copper alloy[J].Corrosion,1995,51(1):1969-2010.
  • 9Jones K,David W H.Prior corrosion and fatigue of 2024-T3 aluminum alloy [J].Corrosion Science.2006,48(10):3109-3122.
  • 10Savoia M.Structural reliability analysis through fuzzy number approach with application to stability [J].Computers and Structures.2002,80(12):1087-1102.

引证文献9

二级引证文献24

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部