G.E.® TRIO II Stage 5 Compressor Rotor Blade K645P13
GE Engines Trio II
Part # K645P13=CK
8130-3 Eligible
8130-3 Eligible
The K645P13 compressor rotor blades enhance air pressure, temperature, and velocity in GE Engine TRIO II systems. Their aerodynamic design promotes smooth airflow, reducing drag and optimizing pressure ratios. Made from high-strength super alloys with a polished coating, these blades are built to endure high engine temperatures and pressures.The K645P13 compressor rotor blades
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Overview
GE Engine TRIO II K645P13 Stage-5 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, K645P13 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 K645P13 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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