Size (CM): 40*40*20

Weright (KG): 15

K47002-35 is a precision-machined aerospace engine high-pressure compressor (HPC) rotor blade, compliant with AS9100D quality standards and FAA/EASA regulations, optimized for CFM56 and IAE V2500 turbofan engines. It accelerates incoming airflow to high pressure for combustion chamber supply, directly enhancing engine thrust output and thermal efficiency across idle, climb, cruise, and takeoff phases.

Crafted from a heat-resistant nickel-based superalloy with a protective aluminide coating, it withstands operating temperatures up to 800°C, extreme centrifugal forces, and high-velocity particle erosion. Weighing 0.18kg with a precision dovetail root design, it enables rapid replacement during compressor hot-section MRO overhauls. FAA Part 25 certified, it is a safety-critical component for engine compression system reliability and performance.