Mechanical properties degradation of (Al-Cu-Li) 2198 alloy due to corrosion exposure

被引:23
作者
Alexopoulos, Nikolaos D. [1 ]
Proiou, Angeliki [1 ]
Dietzel, Wolfgang [2 ]
Blawert, Carsten [2 ]
Heitmann, Volker [2 ]
Zheludkevich, Mikhail [2 ]
Kourkoulis, Stavros K. [3 ]
机构
[1] Univ Aegean, Dept Financial Engn, Chios 82132, Greece
[2] Helmholtz Zentrum Geesthacht, Dept Corros & Surface Technol, Inst Mat Res, D-21502 Geesthacht, Germany
[3] Natl Tech Univ Athens, Dept Mech, Lab Testing & Mat, 9 Heroes Polytechniou Str, Athens 15773, Greece
来源
21ST EUROPEAN CONFERENCE ON FRACTURE, (ECF21) | 2016年 / 2卷
关键词
alloy; 2024; 2198; tension; artificial ageing; exfoliation corrosion; ductility; DEFORMATION; DAMAGE;
D O I
10.1016/j.prostr.2016.06.077
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The present work investigates the corrosion resistance of the innovative Al-Cu-Li (2198) aluminum alloy; a comparison against Al-Cu (2024) alloy is attempted. Tensile specimens were pre-corroded for different exposure times to exfoliation corrosion solution and immediately afterwards they were tested in tension. For small exposure times (< 12 h) small pits could be found on the corroded surfaces; pitting was also noticed at the small side surfaces (thickness) of the tensile specimens. Corrosion exposure seems not to essentially decrease the yield stress of AA2198 even for high exposure times, while this was not the case for AA2024. After heavy corrosion exposure (> 12 h), AA2024 lost almost 30% of its initial ultimate tensile strength, while for AA2198 the respective value was only I11%. Al-Cu-Li alloy shows superior corrosion resistance in terms of maintaining higher percentages of tensile ductility; AA2198 exhibited higher remaining elongation at fracture values due to corrosion degradation for all investigated exposure times. Copyright (C) 2016 The Authors. Published by Elsevier B.V.
引用
收藏
页码:597 / 603
页数:7
相关论文
共 5 条
[1]   The effect of artificial ageing heat treatments on the corrosion-induced hydrogen embrittlement of 2024 (Al-Cu) aluminium alloy [J].
Alexopoulos, Nikolaos D. ;
Velonaki, Zaneta ;
Stergiou, Constantinos I. ;
Kourkoulis, Stavros K. .
CORROSION SCIENCE, 2016, 102 :413-424
[2]   Fatigue behavior of the aeronautical Al-Li (2198) aluminum alloy under constant amplitude loading [J].
Alexopoulos, Nikolaos D. ;
Migklis, Evangelos ;
Stylianos, Antonis ;
Myriounis, Dimitrios P. .
INTERNATIONAL JOURNAL OF FATIGUE, 2013, 56 :95-105
[3]   Plastic flow and ductile rupture of a 2198 Al-Cu-Li aluminum alloy [J].
Chen, Jianqiang ;
Madi, Yazid ;
Morgeneyer, Thilo F. ;
Besson, Jacques .
COMPUTATIONAL MATERIALS SCIENCE, 2011, 50 (04) :1365-1371
[4]   Interaction between anisotropic plastic deformation and damage evolution in Al 2198 sheet metal [J].
Steglich, D. ;
Wafai, H. ;
Besson, J. .
ENGINEERING FRACTURE MECHANICS, 2010, 77 (17) :3501-3518
[5]   Anisotropic Deformation and Damage in Aluminium 2198 T8 Sheets [J].
Steglich, D. ;
Wafai, H. ;
Brocks, W. .
INTERNATIONAL JOURNAL OF DAMAGE MECHANICS, 2010, 19 (02) :131-152