This compressor stator shroud segment is designed for stage 4 applications, providing structural support and vibration damping. It contains gas flow efficiently, reduces leakage, and minimizes blade flutter. Made from super alloys, it features cooling air channels for temperature protection, contributing to the reliable operation of gas turbines.
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Overview
Shroud for stage 4 compressor stator, the shroud segment is a radial structure on both the inner and outer surfaces that acts as a structural support connecting one stage bucket to another for vibration damping and helps contain the flow of gas so that it is utilized efficiently. The shroud segment forms a continuous annular ring around the compressor blades, thus enclosing the working fluid passage. The compressor shroud encloses the blade tip, thus preventing excessive leakage of the working gas and reducing blade-flutter, improving the efficiency and performance of the compressor segment in 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 5129T69P01 plays a crucial role in the reliable operation of the gas turbine.
Features & Benefits
Provides structural support and vibration damping for enhanced compressor performance.
Encloses the working fluid passage to optimize gas flow efficiency.
Prevents excessive leakage of working gas and reduces blade flutter.
Incorporates cooling air channels for protection against high temperatures.
Manufactured from super alloys for durability and resistance to thermal fatigue.
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