DESIGN AND THERMAL ANALYSIS OF A GAS TURBINE ROTOR BLADE

Abstract

In the present work, the principal organizes rotor sharp edge of a
two-arrange gas turbine has been broken down for auxiliary
warm analysis utilizing ANSYS 12, which is a ground-breaking
Finite Element Software. During the time spent getting the warm
anxieties, the temperature conveyance in the rotor sharp edge has
been assessed utilizing this product. The plan highlights of the
turbine section of the gas turbine have been taken from the
primer outline of a power turbine for the boost of a current
turbojet motor. It was seen that in the above outline, the rotor
cutting edges in the wake of being composed were dissected just
for the mechanical anxieties however no assessment of warm
worry was conveyed.