The Rolls-Royce stage-2 turbine rotor blade 23093193 is engineered to maintain uniform axial air velocity through a pressure gradient. Made from high-strength super alloys, it withstands extreme temperatures and mechanical stress, facilitating the creation of high-pressure, high-velocity air essential for thrust generation in engines.
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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.
Features & Benefits
Resistant to oxidation and corrosion at high temperatures
Reduces gas turbine engine downtime
Increased efficiency thus lowering the fuel consumption
Highly reliable on harsh environmental conditions
Technical Information
NIIN
016604981
NSN
2840-01-660-4981
FSCG
2840
FSCG Category
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
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