High Temperature Oxidation/Sulfidation of Superalloy Haynes 230

Monday, May 11, 2015: 11:00 AM
Room 202B (Long Beach Convention and Entertainment Center)
Mr. Manuel Lira , Universidad Autonoma de Nuevo Leon, San Nicolas de los Garza, Mexico
Dr. Facundo Almeraya Calderon , Universidad Autonoma de Nuevo Leon, San Nicolas de los Garza, Mexico
Dr. Patricia Zambrano Robledo , Universidad Autonoma de Nuevo Leon, San Nicolas de los Garza, Mexico
Dr. Citlalli Gaona Tiburcio , Centro de Investigación e Innovación en ingeniería Aeronáutica-FIME-UANL, Apodaca N.L., Mexico
Dr. Alberto Martinez Villafañe , Centro de Investigacion en Materiales avanzados, Chihuahua, Mexico
Inside a combustion chamber on a gas turbine engine in aircrafts at duty exist very aggressive corrosive agents. One of these is sulphur, which can deteriorate the materials and reduce their useful life. In this paper the superalloy Haynes 230 oxidation kinect was determined by thermogravimetry in temperatures range of 600- 800 °C exposed for 24 hrs in a O2/SO2 mix environment. Gain weight vs time, transversal morphology of the corroded specimen and characterization by scanning electronic microscope (SEM) were determined. The superalloy Haynes 230 in such conditions obey a parabolic kinetic oxidation.
See more of: High Temperature and Turbine Materials I
See more of: High Temperature and Turbine Materials