2019
DOI: 10.1016/j.apsusc.2019.04.242
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Influence of combined shot peening and PEO treatment on corrosion fatigue behavior of 7A85 aluminum alloy

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Cited by 44 publications
(18 citation statements)
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“…The study from various researchers has found that the PEO process reduces the fatigue working of aluminum alloys. To overcome this limitation, Ye et al [ 225 ] explored the synergism of a cold working treatment process and a hard coating to improve the fatigue resistance, wear, and corrosion resistance of a 7A85 Al alloy. This alloy is one of the most key materials required by the aviation industry.…”
Section: Applications Of Peomentioning
confidence: 99%
“…The study from various researchers has found that the PEO process reduces the fatigue working of aluminum alloys. To overcome this limitation, Ye et al [ 225 ] explored the synergism of a cold working treatment process and a hard coating to improve the fatigue resistance, wear, and corrosion resistance of a 7A85 Al alloy. This alloy is one of the most key materials required by the aviation industry.…”
Section: Applications Of Peomentioning
confidence: 99%
“…In following paragraphs, a literature review could be seen for fatigue properties of aluminum alloys [4][5][6][7][8][9][10][11][12][13] and aluminum-matrix composites [14][15][16][17]. In addition, some other articles [18][19][20][21][22][23][24][25][26][27][28][29][30][31][32][33][34][35][36][37] have been reviewed for corrosion-fatigue properties of aluminum alloys. Ueno et al [4] studied fatigue properties of Al-Si-Cu alloys in ambient air and vacuum environments.…”
Section: Introductionmentioning
confidence: 99%
“…They revealed that the corrosion potential of the process was greater, compared to milled surface of the material, due to act as a galvanic couple to an adjacent bulk surface. Ye et al [33] studied the effect of combined shot peening and the plasma electrolytic oxidation on the fatigue behavior of the 7A85 aluminum alloy in air and 3.5% NaCl solutions. Their results indicated that one surface treatment reduced the corrosion-fatigue lifetime.…”
Section: Introductionmentioning
confidence: 99%
“…As a result, the Vickers hardness of the surface layer increased by 320 MPa (HV0.05) more than that of the core of specimens. The surface hardening is caused by plastic deformation due to surface compressive stress introduced by sandblasting [15][16][17][18][19]29]. It can be seen from the figure 3 that the surface compressive stress influencing layer has the depth of approximately 175 μm.…”
Section: Surface Roughness (Ra) Resultsmentioning
confidence: 99%