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Fatigue behavior of a 7075-T6 aluminum alloy coated with an electroless Ni–P deposit |
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| Authors: | E.S. Puchi-Cabrera, C. Villalobos-Guti rrez, I. Irausquí n, J. La Barbera-Sosa,G. Mesmacque |
| Affiliation: | aSchool of Metallurgical Engineering and Materials Science, Faculty of Engineering, Universidad Central de Venezuela, Apartado Postal 47885, Los Chaguaramos, Caracas 1045, Venezuela bSchool of Mechanical Engineering, Faculty of Engineering, Universidad Central de Venezuela, Apartado Postal 47885, Los Chaguaramos, Caracas 1041, Venezuela cDepartment of Industrial Technology, Universidad Simón Bolívar, Sede del Litoral, Postal Address 89000, Caracas 1080, Venezuela dLaboratoire de Mécanique de Lille, Université de Lille 1, Mécanique des Materiaux, UMR CNRS 8107, Villeneuve D’Ascq, 59650, France |
| Abstract: | An investigation has been carried out in order to study the fatigue and corrosion–fatigue behavior of a 7075-T6 aluminum alloy coated with an electroless Ni–P (EN) deposit, in the as-plated condition, of approximately 38–40 μm in thickness and a high P content, of approximately 18 wt%. The results obtained, show that the EN coating can give rise to a significant improvement in the fatigue and corrosion–fatigue performance of the substrate, depending on the testing conditions. When the coated system is tested in air, it is observed that the increase in fatigue properties decreases as the alternating stress applied to the material increases. At stresses of the order of 0.4 σ0.2% the increase in fatigue life is more than about 100%. However, as the stress increases to values in the range of 0.7 σ0.2%, no improvement in the fatigue performance of the system is observed and the behavior is similar to that of the uncoated substrate. Under corrosion–fatigue conditions, the fatigue life is observed to increase between approximately 60% and 70%, depending on the stress applied. It is shown that fatigue cracks are associated with nodular-like defects present on the surface of the coated samples. The deleterious effect of such defects seems to be more pronounced as the alternating stress applied to the material increases. A crude estimate of the yield strength of the EN coating from tensile measurements indicates that such a parameter is in the range of 3.8 GPa, in agreement with the computation of the absolute hardness of the deposit, of about 4 GPa, by means of Meyer’s law. It is also shown that the EN deposit has a very good adhesion to the substrate even when the system is subjected to tensile stresses greater than the yield strength. Such characteristics as well as the higher mechanical properties of the EN coating in comparison with the aluminum alloy substrate and the preservation of its integrity during fatigue testing contribute to the better fatigue performance of the coated system. |
| Keywords: | Electroless Ni–P coating 7075-T6 aluminum alloy Fatigue and corrosion–fatigue properties Absolute hardness Fractographic analysis |
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