MODELING OF CORROSION PILLOWING IN LAP JOINTS MADE OF LY12CZ

被引:0
|
作者
Yu Dazhao [1 ]
Chen Yueliang [1 ]
Gao Yong [1 ]
Jia Zhonghu [1 ]
Liu Wenlin [1 ]
机构
[1] Naval Aeronaut Engn Inst, Yantai, Peoples R China
关键词
lap joint; corrosion pillowing; finite element analysis; structural integrity; stress field;
D O I
暂无
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Finite element techniques were used to determine the effect of pillowing stress on lap joints. The stress caused by the internal pressure, the contacts between the fastener and skin, and geometrical nonlinearity were taken into account. The results show that corrosion pillowing can significantly increase the stress in a lap joint for material loss below the detection limit of current nondestructive inspection techniques, thus increasing the risk of premature cracking. In addition, the analyses show that the locations of maximum stress of lap joint will change with the material loss increases. Simulating the effect of corrosion on lap joint only by reducing the panel thickness will result in nonconservative life estimates if corrosion pillowing is ignored.
引用
收藏
页码:1307 / 1310
页数:4
相关论文
共 50 条
  • [21] GALVANIC CORROSION BETWEEN GRAPHITE EPOXY COMPOSITE MATERIALS AND LY12CZ ALUMINUM ALLOY
    F.Lu
    W.Y.Shen
    J.G. Li and W.D. Zhen(Beijing Institute of Aeronautical Materials
    Acta Metallurgica Sinica(English Letters), 1996, (06) : 669 - 673
  • [22] Galvanic corrosion between graphite epoxy composite materials and LY12CZ aluminum alloy
    Lu, F.
    Shen, W.Y.
    Li, J.G.
    Zhen, W.D.
    Acta Metallurgica Sinica Series A, Physical Metallurgy & Materials Science, 1996, 9 (06): : 669 - 673
  • [23] LY12CZ的腐蚀性能研究
    朱延波
    龙霓东
    航空精密制造技术, 2011, 47 (01) : 38 - 40
  • [24] Research on Corrosion Fractal Character of LY12CZ Aluminum Alloy Based on Image Processing Technique
    Mu, ZhiTao
    Zhu, ZuoTao
    Chen, DingHai
    Zhang, FuGao
    NEW MATERIALS AND ADVANCED MATERIALS, PTS 1 AND 2, 2011, 152-153 : 1691 - +
  • [25] GALVANIC CORROSION AND PROTECTION OF GECM/LY12CZ COUPLES UNDER DIFFERENT ATMOSPHERIC EXPOSURE CONDITIONS
    F.Lu
    Q.P.Zhong
    C.X.Cao
    ActaMetallurgicaSinica(EnglishLetters), 2003, (01) : 41 - 45
  • [26] Research on Aircraft LY12CZ Aluminum Alloy Corrosion Damage Prediction Based on ARIMA Model
    Liu Zhi-guo
    Mu Zhi-tao
    ADVANCED DESIGN TECHNOLOGY, PTS 1-3, 2011, 308-310 : 1016 - 1022
  • [27] Probabilistic Study on Corrosion Damage Distribution and Fatigue Lives of LY12CZ Aluminum Alloy Structure
    Yu, Dazhao
    Chen, Yueliang
    Yong, Zhang
    Fan Qinghe
    MECHANICAL, MATERIALS AND MANUFACTURING ENGINEERING, PTS 1-3, 2011, 66-68 : 594 - +
  • [28] Novel accelerated corrosion test for LY12CZ and LC4CS aluminum alloys
    Cai Jian-ping
    Liu Ming
    TRANSACTIONS OF NONFERROUS METALS SOCIETY OF CHINA, 2006, 16 : S1415 - S1418
  • [29] Novel accelerated corrosion test for LY12CZ and LC4CS aluminum alloys
    蔡健平
    刘明
    Transactions of Nonferrous Metals Society of China, 2006, (S3) : 1415 - 1418
  • [30] Galvanic corrosion and protection of GECM/LY12CZ couples under different atmospheric exposure conditions
    Lu, F.
    Zhong, Q.P.
    Cao, C.X.
    Acta Metallurgica Sinica (English Letters), 2003, 16 (01) : 41 - 45