G.E. 4124T43P01 Stage 2 High Pressure Turbine Blade Shroud
GE Engine Services
Part # 4124T43P01=CZ
8130-3 Eligible
8130-3 Eligible
This high-pressure turbine blade shroud provides structural support between turbine stages, minimizing gas leakage and blade flutter. It features cooling air channels for temperature protection and is made from super alloys for enhanced thermal and fatigue resistance, contributing to the effective operation of gas turbines. Part number 4124T43P01 is essential for performance.Th
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Overview
The shroud acts as a structural support connecting one stage bucket to another for vibration damping and helps contain the flow of high-pressure gas so that the gas is utilized efficiently. The Stage 2 HPT shroud encloses the blade tip, thus preventing excessive leakage of high-pressure gas and reducing blade-flutter, improving the efficiency and performance of the turbine. The shroud incorporates cooling air channels, protecting it from high-temperature damage. Manufactured from super alloys, the shroud has excellent thermal and fatigue-resistant properties. Overall, part number 4124T43P01 plays a crucial role in the reliable operation of the gas turbine.
Features & Benefits
Provides structural support and vibration damping between turbine stages
Prevents excessive leakage of high-pressure gas, improving turbine efficiency
Reduces blade flutter for enhanced performance
Incorporates cooling air channels to protect against high-temperature damage
Manufactured from super alloys for excellent thermal and fatigue resistance
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