The G.E. Stage 2 Low Pressure Turbine Blade 1536M22P03 is engineered for low pressure ratio applications, enhancing aerodynamic efficiency and exhaust energy recovery. Designed to endure extreme conditions, it features high-strength super alloys and an internal cooling flow to manage mechanical stress and withstand high temperatures during operation.
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Overview
GE Engines TRIO II Low Pressure Stage-2 Turbine Blades 1536M22P03 are specifically designed for low pressure ratio operation to provide high aerodynamic efficiency, recover exhaust energy, and minimize back pressure. These 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 those circumstances, 1536M22P03 turbine blade manages mechanical stress and also transfers heat to an internal cooling flow in order to survive in these conditions. The high-resistance super polished high-pressure stage-2 turbine blade 1536M22P03 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
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
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