Design and analysis of a high-pressure turbine blade in a jet engine using advanced materials

In this study, the use of Inconel 625, Palladium alloy and Titanium alloy have been done in jet turbine blade. The modelling of the turbine blade was done in Solidworks 16.0 software and its simulation was done under numerical computational method using Ansys 16.0 software. The tests conducted in the software were the equivalent stress (von misses stress), equivalent strain, and total deformation. Three types of material configuration were tested and compared: using only Ni-based alloy, using Ni-based alloy with Titanium and using Ni-based alloy along with Pd-alloy at high stress zones of the blade.