A DESIGN AND ANALYSIS OF GAS TURBINE BLADE PROFILES USING DIFFERENT MATERIALS

Abstract

Right now, one of the most effective sources of turbo machinery is gas turbines. Numerous industries, 
including manufacturing, aircraft, homes, and small businesses, may benefit from this technology. The 
selection of materials, turbine rotor blade vibration management, and blade shapes are all difficult tasks 
for gas turbine engines. These parameters have a major impact on stress deformation and structural 
performance. Analysis has been done on the overall heat flow, the directional distortions of the turbine 
blades, and the thermal inaccuracy that results from the heat and centrifugal stresses interacting. 
Furthermore, thermal loading is the cause of the temperature flow. To determine which material is best 
for a turbine blade, the performance of three different materials—Inconel 718, titanium T6, and 
SS316—is tested.