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 in | International journal of fracture Vol. 240; no. 2; pp. 209 - 220 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
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. |
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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 |
Author_xml | – sequence: 1 givenname: Benaïssa orcidid: 0000-0001-6988-9133 surname: Malek fullname: Malek, Benaïssa email: bnssmalek@gmail.com organization: Université de Toulouse, Institut Clément Ader (ICA), UMR CNRS 5312, UPS/INSA/ISAE/Mines Albi – sequence: 2 givenname: Michel surname: Chaussumier fullname: Chaussumier, Michel organization: Université de Toulouse, Institut Clément Ader (ICA), UMR CNRS 5312, UPS/INSA/ISAE/Mines Albi – sequence: 3 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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Keywords | Fatigue Tension Anodizing 2618-T851 Torsion |
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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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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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