23093193 Stage 2 Turbine Rotor Blade Shroud

OVERVIEW

The 23093193 Rolls-Royce stage-2 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 stage-2 turbine rotor blade 23093193 is fabricated from high strength super alloys that can withstand engine operating temperature. 23093193 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 23093193 turbine blade manages mechanical stress and also transfers heat to survive in these conditions.