Influence of corrosion on the fatigue properties of Al 7075-T6

被引:0
作者
Du, ML [1 ]
Chiang, FP
Kagwade, SV
Clayton, CR
机构
[1] SUNY Stony Brook, Dept Mech Engn, Stony Brook, NY 11794 USA
[2] SUNY Stony Brook, Dept Mat Sci & Engn, Stony Brook, NY 11794 USA
关键词
fatigue; corrosion; damage; surface roughness; laser speckle; correlation coefficient;
D O I
暂无
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Chloride ion attack on Al 7075-76 in aqueous hydrochloric acid leads to localized corrosion and subsequent initiation of fatigue cracks on the surface. Fitting is observed when the specimen is exposed to a corrosive environment. Microcracks, voids, extrusions, and intrusions are then formed during the fatigue process. From a global viewpoint, all of the corrosion and fatigue damage appears to be randomly oriented, resulting in a change in the surface roughness. The Laser Speckle Sensor technique is used to detect the minute surface texture change, associated with the damage caused by corrosion and fatigue. Nonuniform surface roughness is observed due to corrosion. The corrosion pits tend to coalesce along the rolling direction. The change in surface roughness is significant around the crack tip during the fatigue process. As a result there are synergistic activities; the surface roughness caused by corrosion and fatigue leads to crack initiation, and the crack growth further increases surface roughness.
引用
收藏
页码:260 / 268
页数:9
相关论文
共 50 条
[21]   Fatigue crack growth in the micro to large scale of 7075-T6 Al sheets at different R ratios [J].
Tang, K. K. ;
Berto, F. ;
Wu, H. .
THEORETICAL AND APPLIED FRACTURE MECHANICS, 2016, 83 :93-104
[22]   Fatigue data interpretation of 7075-T6 Al sheets by energy density factor in a dual scale model [J].
Tang, K. K. ;
Wu, H. ;
Berto, F. .
THEORETICAL AND APPLIED FRACTURE MECHANICS, 2015, 79 :98-104
[23]   Ultrasonic and Conventional Fatigue Endurance of Aeronautical Aluminum Alloy 7075-T6, with Artificial and Induced Pre-Corrosion [J].
Zuniga Tello, Ishvari F. ;
Milkovic, Marijana ;
Dominguez Almaraz, Gonzalo M. ;
Gubeljak, Nenad .
METALS, 2020, 10 (08) :1-17
[24]   Equivalent crack size model for pre-corrosion fatigue life prediction of aluminum alloy 7075-T6 [J].
Huang, Yongfang ;
Ye, Xubin ;
Hu, Benrun ;
Chen, Lijie .
INTERNATIONAL JOURNAL OF FATIGUE, 2016, 88 :217-226
[25]   Study of the influence of the RRA thermal treatment and plasma nitriding on corrosion behavior of 7075-T6 aluminum alloy [J].
Savonov, Graziela da Silva ;
Galvao Camarinha, Maria Gabriela ;
Rocha, Leticia Oliveira ;
Ribeiro Barboza, Miguel Justino ;
Martins, Gislene Valdete ;
Pereira Reis, Danieli Aparecida .
SURFACE & COATINGS TECHNOLOGY, 2019, 374 :736-744
[26]   Influence of pin imperfections on the tensile and fatigue behaviour of AA 7075-T6 friction stir lap welds [J].
M. Balakrishnan ;
C. Leitão ;
E. Arruti ;
E. Aldanondo ;
D. M. Rodrigues .
The International Journal of Advanced Manufacturing Technology, 2018, 97 :3129-3139
[27]   Influence of pin imperfections on the tensile and fatigue behaviour of AA 7075-T6 friction stir lap welds [J].
Balakrishnan, M. ;
Leitao, C. ;
Arruti, E. ;
Aldanondo, E. ;
Rodrigues, D. M. .
INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2018, 97 (5-8) :3129-3139
[28]   On the fatigue durability of clad 7075-T6 aluminium alloy bonded joints representative of aircraft repair [J].
Harman, A. B. ;
Rider, A. N. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2013, 44 :144-156
[29]   Study of Vibration-Ultrasonic Combined Fatigue on 7075-T6 Aluminum Alloy [J].
Zhao, Ziyu ;
Tang, Sen ;
Chen, Mingsan ;
Liu, Yongjie ;
He, Chao ;
Xu, Bo ;
Wang, Chong ;
Wang, Qingyuan .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2025, 48 (01) :231-243
[30]   The influence of surface enhancement by low plasticity burnishing on the corrosion fatigue performance of AA7075-T6 [J].
Prevéy, PS ;
Cammett, JT .
INTERNATIONAL JOURNAL OF FATIGUE, 2004, 26 (09) :975-982