Hot Corrosion Behaviour by Electrochemical Techniques of Inconel 718 in Aeronautical Applications

Monday, May 6, 2019: 9:30 AM
Redwood 6 (Nugget Casino Resort)
Mr. J.M Jaquez , Universidad Autonoma de Nuevo Leon, Apocada, Nuevo León, Mexico
Dr. J.L Tristancho , Universidad Tecnológica de Pereira, Pereira, Colombia
Dr. Citllalli Gaona , Universidad Autonoma de Nuevo Leon, Apocada, Nuevo León, Mexico
Dr. F. Estupiñan , Universidad Autonoma de Nuevo Leon, Apocada, Nuevo León, Mexico
Dr. Patricia Zambrano , Universidad Autonoma de Nuevo Leon, Apocada, Nuevo León, Mexico
Dr. José Cabral , Universidad Autonoma de Nuevo Leon, Apocada, Nuevo León, Mexico
Dr. Facundo Almeraya , Universidad Autonoma de Nuevo Leon, Apocada, Nuevo León, Mexico
Aeronautical industry needs materials that possess the ability to maintain their properties at high temperatures, that materials are high-temperature materials, superalloys, used on components of turbines. Aeroengines depends of nickel-based superalloys for hottest sections due to the resistance to fatigue and creep in operative conditions. Considering the operative temperatures of aeroengines, hot corrosion must be investigated to determinate the behaviour of the superalloy, in this case Inconel 718 in presence of Na2SO4, NaVO3 and 80V2O5-20Na2SO4. The results showed that the salts aggressivity increased with temperature, leading the material to corrosion. 80V2O5-20Na2SO4 was most aggressive salt. Na2SO4 and NaVO3 increase corrosion rate while temperature increases. The electrochemical results coincide with SEM analysis.
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