G.E. 1538M90P22 Stage-1 High Pressure Turbine Blade
GE Engines TRIO II
Part # 1538M90P22=CK
8130-3 Eligible
8130-3 Eligible
The high pressure turbine blade 1538M90P22 is designed for stage-1 applications, effectively extracting energy from extreme temperature and pressure conditions. Constructed from high-strength super alloys, it manages mechanical stress and facilitates internal cooling, ensuring durability during operation in demanding environments.The high pressure turbine blade 1538M90P22 is de
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Overview
GE's stage-1 high pressure turbine blades 1538M90P22 are responsible for extracting energy from high pressure and temperature. Turbine blades must operate under extreme circumstances, such as rotating at higher RPM through gas streams that may have higher temperatures than the blade's melting point. In such circumstances 1538M90P22 turbine blade manages mechanical stress and also transfers heat to an internal cooling flow in order to survive in these conditions. This high-resistance super polished high-pressure stage-1 turbine blade 1538M90P22 is fabricated from high strength super alloys that can withstand engine operating temperature.
Features & Benefits
Resistant to oxidation and corrosion at high temperatures
Reduces gas turbine engine downtime
Coated with thermal barrier coating
Increased efficiency thus lowering the fuel consumption
Highly reliable on harsh environmental conditions
Technical Information
ATA Number
72
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
ATA Group
Power Plant
ATA Section
HIGH PRESSURE TURBINE SHROUD AND 1ST-STAGE LOW PRESSURE TURBINE NOZZLE
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