Effect of anodization and loading on fatigue life of 2618-T851 aluminum alloy

Anodizing process is largely performed on aluminum alloys to enhance corrosion and wear resistances. However, this process can significantly reduce the fatigue resistance of aluminum alloys depending on the alloy and the process parameters. This paper deals with the influence of anodizing process on...

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Published inInternational journal of fracture Vol. 240; no. 2; pp. 209 - 220
Main Authors Malek, Benaïssa, Chaussumier, Michel, Mabru, Catherine
Format Journal Article
LanguageEnglish
Published Dordrecht Springer Netherlands 01.04.2023
Springer Nature B.V
Springer Verlag
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Abstract Anodizing process is largely performed on aluminum alloys to enhance corrosion and wear resistances. However, this process can significantly reduce the fatigue resistance of aluminum alloys depending on the alloy and the process parameters. This paper deals with the influence of anodizing process on fatigue resistance of the aeronautical aluminum alloy 2618-T851. The anodic film has been characterized after each step using scanning electron microscopy (SEM). This analysis showed that the anodic layer was crazed just after impregnation operation with micro-cracks extending from the surface up to half the anodic layer. Simultaneously, uniaxial fatigue tests under tension or torsion loadings have been conducted in order to evaluate the effect of each process step in relation with loading nature. The results showed that the anodizing step has a detrimental effect on fatigue life of 2618 alloy when specimens are subjected to tensile loading. However, anodizing process has no effect on fatigue life under torsion loading. Fractographic observations have been conducted in order to get an insight on the mechanisms involved in each case.
AbstractList Anodizing process is largely performed on aluminum alloys to enhance corrosion and wear resistances. However, this process can significantly reduce the fatigue resistance of aluminum alloys depending on the alloy and the process parameters. This paper deals with the influence of anodizing process on fatigue resistance of the aeronautical aluminum alloy 2618-T851. The anodic film has been characterized after each step using scanning electron microscopy (SEM). This analysis showed that the anodic layer was crazed just after impregnation operation with micro-cracks extending from the surface up to half the anodic layer. Simultaneously, uniaxial fatigue tests under tension or torsion loadings have been conducted in order to evaluate the effect of each process step in relation with loading nature. The results showed that the anodizing step has a detrimental effect on fatigue life of 2618 alloy when specimens are subjected to tensile loading. However, anodizing process has no effect on fatigue life under torsion loading. Fractographic observations have been conducted in order to get an insight on the mechanisms involved in each case.
Anodizing process is largely performed onaluminum alloys to enhance corrosion and wearresistances. However, this process can significantlyreduce the fatigue resistance of aluminum alloysdepending on the alloy and the process parameters.This paper deals with the influence of anodizingprocess on fatigue resistance of the aeronauticalaluminum alloy 2618-T851. The anodic film has beencharacterized after each step using scanning electronmicroscopy (SEM). This analysis showed that theanodic layer was crazed just after impregnationoperation with micro-cracks extending from thesurface up to half the anodic layer. Simultaneously,uniaxial fatigue tests under tension or torsion loadingshave been conducted in order to evaluate the effect ofeach process step in relation with loading nature. Theresults showed that the anodizing step has a detrimentaleffect on fatigue life of 2618 alloy when specimensare subjected to tensile loading. However, anodizingprocess has no effect on fatigue life under torsionloading. Fractographic observations have been conductedin order to get an insight on the mechanismsinvolved in each case.
Author Chaussumier, Michel
Malek, Benaïssa
Mabru, Catherine
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  organization: Université de Toulouse, Institut Clément Ader (ICA), UMR CNRS 5312, UPS/INSA/ISAE/Mines Albi
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  givenname: Michel
  surname: Chaussumier
  fullname: Chaussumier, Michel
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  givenname: Catherine
  surname: Mabru
  fullname: Mabru, Catherine
  organization: Université de Toulouse, Institut Clément Ader (ICA), UMR CNRS 5312, UPS/INSA/ISAE/Mines Albi
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CitedBy_id crossref_primary_10_1016_j_vacuum_2023_112911
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Issue 2
Keywords Fatigue
Tension
Anodizing
2618-T851
Torsion
Language English
License Distributed under a Creative Commons Attribution 4.0 International License: http://creativecommons.org/licenses/by/4.0
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Snippet Anodizing process is largely performed on aluminum alloys to enhance corrosion and wear resistances. However, this process can significantly reduce the fatigue...
Anodizing process is largely performed onaluminum alloys to enhance corrosion and wearresistances. However, this process can significantlyreduce the fatigue...
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StartPage 209
SubjectTerms Alloys
Aluminum alloys
Aluminum base alloys
Anodizing
Automotive Engineering
Characterization and Evaluation of Materials
Civil Engineering
Classical Mechanics
Corrosion fatigue
Corrosion resistance
Corrosive wear
Engineering
Engineering Sciences
Fatigue cracks
Fatigue life
Fatigue strength
Fatigue tests
Mechanical Engineering
Mechanics
Metal fatigue
Microcracks
Original Paper
Process parameters
Structural mechanics
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Title Effect of anodization and loading on fatigue life of 2618-T851 aluminum alloy
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