G.E.® 4124T42P09 Stage 1 High Pressure Turbine Shroud
GE Engine Services
Part # 4124T42P09=CZ
8130-3 Eligible
8130-3 Eligible
This high-pressure turbine shroud provides structural support between turbine stages, minimizing gas leakage and reducing blade flutter. It features cooling air channels for thermal protection and is made from super alloys for enhanced durability. The shroud is essential for maintaining the performance and reliability of gas turbines.This high-pressure turbine shroud provides s
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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 1 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 the shroud from high-temperature damage. Manufactured from super alloys the shroud has excellent thermal and fatigue resistant properties. Overall, part number 4124T42P09 shroud 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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