C20 2nd Stage Nozzle

The C20 2nd Stage Nozzle is a critical hot-section component designed for Rolls-Royce M250/C20 series gas turbine engines. Positioned between the first-stage and second-stage turbine rotors, the second-stage nozzle directs and accelerates high-temperature combustion gases onto the second-stage turbine blades at the correct angle, maximizing energy transfer, engine efficiency, and overall performance.

Manufactured from premium nickel-based superalloys, the nozzle is engineered to withstand extreme operating temperatures, thermal cycling, oxidation, and corrosion. Precision machining and rigorous quality inspections ensure excellent dimensional accuracy, reliable airflow characteristics, and long service life, making it an ideal choice for engine overhaul, repair, and MRO applications.

Features

• Designed for Rolls-Royce M250/C20 series gas turbine engines

• Precision-engineered second-stage turbine nozzle

• Manufactured from high-temperature nickel-based superalloys

• Excellent resistance to thermal fatigue, oxidation, and corrosion

• Optimized vane geometry for efficient gas flow

• High dimensional accuracy for reliable installation

• Suitable for OEM replacement and aerospace MRO applications

Applications

• Rolls-Royce M250-C20 series turbine engines

• Helicopter engine overhaul and maintenance

• Aerospace MRO facilities

• Commercial and military aviation support