Adaptive work performance analysis of INCONEL-738 for use in Gas turbine Blade and its application in Turbo machinery

Abstract

Turbo machinery is basically Describe in mechanical engineering, there Describe turbine, Compressor, diffuser, combustion chamber and nozzle. The IN-738 is nickel base super alloy. This is high performance super alloy, this super alloy produce high temperature strength with high strength. In this experiment test Tensile and thermal expansion are concluded, In order to perform successfully and economically at high temperatures, a material must have at least two essential characteristics: it must be strong, since increasing temperature tends to reduce strength, and it must have resistance to its environment. Since oxidation and corrosion attack also increase with temperature.
Keywords- IN-738; Ni-based Super alloy; Turbo machine; Gas turbine materials; alloys; tensile Test; thermal expansion