Genting Lanco Power Private Ltd
• Fielded and documented gas turbine, combustion chamber, steam turbine, and heat recovery system.
• Designed and Analyzed a gas turbine blade to determine the best composite material.
• Simulated the gas turbine blade with four materials to study the thermal analysis coupled with structural analysis.
• Investigated the temperature, equivalent stress, total deformation, and factor of safety to determine the best composite material.
Findings
• Gas turbine blades are subjected to high tangential, axial, and centrifugal forces during their functioning, and their design requires the greatest attention to detail.
• The leading edge of the turbine blade will receive more hot gases when compared to the trailing edge.
• Analysed Haste Alloy X, Inconel 625, N155, and Titanium t6 and determined that Inconel 625 is the best-suited material for a gas turbine blade.
Haste Alloy simulation results
Inconel simulation results
N155 simulation results
Titanium t6 simulation results
