Determination of Fatigue Analysis of Compressor Disc in Gas Turbine

An abaqus software is used to evaluate fatigue testing of tie bolt holes in a typical gas turbine compressor disc. The material properties needed for the disk are taken as a grade TI-8AL-1MO-1V Titanium alloy. The research focus is on the impact of Uniaxial loading and cyclic rotation speed is subjected to the disc. A solution is fully obtained under uniaxial loading for a disc, numerical analysis measures the problems for the disc.