Corrosion damage evolution and mechanical properties of carbon fiber reinforced aluminum laminate

被引:16
作者
Wu, Xin-tong [1 ,2 ]
Zhan, Li-hua [1 ,2 ]
Huang, Ming-hui [1 ,2 ]
Zhao, Xing [1 ,2 ]
Wang, Xun [1 ,2 ]
Zhao, Guo-qing [1 ,2 ]
机构
[1] Cent South Univ, State Key Lab High Performance Complex Mfg, Changsha 410083, Peoples R China
[2] Cent South Univ, Sch Mech & Elect Engn, Changsha 410083, Peoples R China
基金
中国国家自然科学基金;
关键词
carbon fiber reinforced aluminum laminate; galvanic corrosion; electrochemistry; interlaminar shear strength; aluminum alloy; EXFOLIATION CORROSION; MICROSTRUCTURE; BEHAVIOR; PROTECTION; ALLOY;
D O I
10.1007/s11771-021-4635-8
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
Fiber metal laminates (FMLs), a kind of lightweight material with excellent comprehensive performance, have been successfully applied in aerospace. FMLs reinforced with carbon fiber have better mechanical properties than those with glass or aramid fiber. However, carbon fiber binding metal may lead to galvanic corrosion which limits its application. In this paper, electrochemical methods, optical microscope and scanning electron microscope were used to analyze the corrosion evolution of carbon fiber reinforced aluminum laminate (CARALL) in corrosive environment and explore anti-corrosion ways to protect CARALL. The results show that the connection between carbon fiber and aluminum alloy changes electric potential, causing galvanic corrosion. The galvanic corrosion will obviously accelerate CARALL corroded in solution, leading to a 72.1% decrease in interlaminar shear strength, and the crevice corrosion has a greater impact on CARALL resulting in delamination. The reduction of interlaminar shear strength has a similar linear relationship with the corrosion time. In addition, the adhesive layers between carbon fiber and aluminum alloy cannot protect CARALL, while side edge protection can effectively slow down corrosion rate. Therefore, the exposed edges should be coated with anti-corrosion painting. CARALL has the potential to be used for aerospace components.
引用
收藏
页码:657 / 668
页数:12
相关论文
共 35 条
[1]  
Andrzej K., 2019, COMPOSITES B, V176, P1
[2]   Investigation of fatigue crack growth rate in CARALL, ARALL and GLARE [J].
Asghar, W. ;
Nasir, M. A. ;
Qayyum, F. ;
Shah, M. ;
Azeem, M. ;
Nauman, S. ;
Khushnood, S. .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2017, 40 (07) :1086-1100
[3]  
BIENIAS J, 2013, 19 INT C COMP MAT, P1
[4]   An experimental review on the mechanical properties and hygrothermal behaviour of fibre metal laminates [J].
Chandrasekar, M. ;
Ishak, M. R. ;
Jawaid, M. ;
Leman, Z. ;
Sapuan, S. M. .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2017, 36 (01) :72-82
[5]   Pullulan as a potent green inhibitor for corrosion mitigation of aluminum composite: Electrochemical and surface studies [J].
Charitha, B. P. ;
Rao, Padmalatha .
INTERNATIONAL JOURNAL OF BIOLOGICAL MACROMOLECULES, 2018, 112 :461-472
[6]  
Chen Y., 2020, ADV POLYM TECH, V4, P1
[7]   Corrosion behavior and mechanical properties of cold metal transfer welded dissimilar AA7075-AA5754 alloys [J].
Comez, Nilay ;
Durmus, Hulya .
JOURNAL OF CENTRAL SOUTH UNIVERSITY, 2020, 27 (01) :18-26
[8]   On the effect of glass and carbon fiber hybridization in fiber metal laminates: Analytical, numerical and experimental investigation [J].
Dadej, Konrad ;
Bienias, Jaroslaw ;
Surowska, Barbara .
COMPOSITE STRUCTURES, 2019, 220 :250-260
[9]   Residual fatigue life of carbon fibre aluminium laminates [J].
Dadej, Konrad ;
Bienias, Jaroslaw ;
Surowska, Barbara .
INTERNATIONAL JOURNAL OF FATIGUE, 2017, 100 :94-104
[10]  
Dhaliwal G., 2016, J Dyn Behav Mater, V2, P181, DOI DOI 10.1007/S40870-016-0083-1