On the effect of coatings on the tensile and fatigue properties of 7075-T6 aluminum alloy monitored with acoustic Emission (AE): Towards lifetime estimation

被引:10
作者
Vie, T. [1 ]
Deschanel, S. [1 ]
Godin, N. [1 ]
Normand, B. [1 ]
机构
[1] Univ Lyon, Univ Claude Bernard Lyon 1, INSA Lyon, CNRS,MATEIS,UMR5510, F-69621 Villeurbanne, France
关键词
Fatigue; Acoustic Emission; Structural Health Monitoring; Aluminium alloy; Coating; CRACK-GROWTH; PLASTIC-DEFORMATION; ANODIZING PROCESS; STAINLESS-STEEL; BEHAVIOR; MICRO; IDENTIFICATION; PERFORMANCE; STRENGTH; DAMAGE;
D O I
10.1016/j.ijfatigue.2023.107578
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Acoustic Emission (AE) is used to monitor the fatigue behaviour of specimens made of aluminium alloy 7075-T6 and covered with different coating combinations: anodic oxidation (alumina) -primer layer (organic coating) -topcoat layer (organic coating)). AE monitoring allows to understand and differentiate the processes and damage mechanisms in action during fatigue for all types of specimens. The type of coating applied has a significant influence on the damage process and the fatigue lifetime of the material. AE-based indicators are defined to assess the overall damage state of the specimens during fatigue testing. Some indicators are based on the distinction of the acoustic activity acquired during the loading and unloading phases of the cycles. As an example, the joint analysis of these indicators on anodized samples allows to highlight characteristic times ranging from 15% to 70% of the specimen's lifetime. The early time at 15% is related to the saturation of cracking of the oxide layer during the first cycles of fatigue tests. By 70% of failure life, the AE activity correlates with the propagation of the main crack in the substrate, assisted by brittle fracture of the surrounding oxide layer. These specific times provide information on the Remaining Useful Lifetime (RUL) of the material and could be used to anticipate future failure.
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页数:13
相关论文
共 56 条
[11]   In situ observation of the cracking behavior of TiN coating on 304 stainless steel subjected to tensile strain [J].
Chen, BF ;
Hwang, J ;
Yu, GP ;
Huang, JH .
THIN SOLID FILMS, 1999, 352 (1-2) :173-178
[12]   Effect of anodic oxidation on fatigue performance of 7075-T6 alloy [J].
Cirik, E. ;
Genel, K. .
SURFACE & COATINGS TECHNOLOGY, 2008, 202 (21) :5190-5201
[13]   ACOUSTIC-EMISSION DURING THE PLASTIC-DEFORMATION OF ALUMINUM ALLOY-2024 AND ALLOY-2124 [J].
COUSLAND, SM ;
SCALA, CM .
MATERIALS SCIENCE AND ENGINEERING, 1983, 57 (01) :23-29
[14]  
Cree A. M., 1997, Surface Engineering, V13, P51
[15]  
Daniel I.M., 1998, Nondestructive Testing and Evaluation, V14, P71
[16]   Recent developments in advanced aircraft aluminium alloys [J].
Dursun, Tolga ;
Soutis, Costas .
MATERIALS & DESIGN, 2014, 56 :862-871
[17]  
El May W., 2013, THESIS INSA LYON LYO
[18]   Computational micromechanics analysis of cyclic crack-tip behavior for micro structurally small cracks in dual-phase Al-Si alloys [J].
Fan, JH ;
McDowell, DL ;
Horstemeyer, MF ;
Gall, K .
ENGINEERING FRACTURE MECHANICS, 2001, 68 (15) :1687-1706
[20]   Contribution of AE analysis in order to evaluate time to failure of ceramic matrix composites [J].
Godin, Nathalie ;
Reynaud, Pascal ;
Fantozzi, Gilbert .
ENGINEERING FRACTURE MECHANICS, 2019, 210 :452-469