G.E.® TRIO II Stage 4 Compressor Rotor Blade K644P13
GE Engines Trio II
Part # K644P13=CK
8130-3 Eligible
8130-3 Eligible
The K644P13 compressor rotor blades are designed for GE Engine TRIO II systems, enhancing air pressure, temperature, and velocity. Their aerodynamic shape promotes smooth airflow, reducing drag. Made from high-strength super alloys with a polished coating, these blades are built to endure high engine temperatures and pressures, optimizing compressor performance.The K644P13 comp
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Overview
GE Engine TRIO II K644P13 Stage-4 compressor rotor blades increase the pressure and temperature of the air passing through. By virtue of their motion, they also increase the velocity slightly. The shape of the blade allows for a smooth flow of air over the surface, which reduces drag and increases the efficiency of the compressor. Additionally, K644P13 compressor rotor blades are designed to optimize the pressure ratio of the compressor, which can improve the performance of the overall system. The rotor compressor blade K644P13 is fabricated from high strength super alloys with super polished protection coating that can withstand engine operating temperature and pressure.
Features & Benefits
Reduces gas turbine engine downtime
Lowers the fouling rate
Resilient finish prevents the collection of dirt and debris in the blades
Increased water-washing intervals for gas turbine compressors
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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