G.E. 1881M52G31 Stage 2 High Pressure Turbine Rotor Blade

The 1881M52G31 stage-2 GE engine high pressure turbine rotor blade is designed to provide a pressure gradient along its length to ensure that the air is maintained at a suitably uniform axial velocity. The air stream's centrifugal force is countered by the rotor's centrifugal action due to the increased pressure at the tip. This high-resistance super polished high-pressure turbine rotor blade 1881M52G31 is fabricated from high strength super alloys that can withstand engine operating temperature. 1881M52G31 stage-2 turbine rotor blades work to create the high-pressure and high-velocity air that is necessary for the engine to produce thrust. In such circumstances 1881M52G31 turbine blade manages mechanical stress and also transfers heat to survive in these conditions.