CM247 high-temperature alloy powder
CM247 is a γ′ phase-strengthened nickel-based superalloy with excellent high-temperature strength, creep resistance, oxidation resistance, and hot corrosion resistance. It is widely used in extreme high-temperature environments such as aero-engine turbine blades and gas turbine hot-end components. Its high volume fraction of γ′ phase (≥40%) and stable carbide distribution enable it to maintain stable mechanical properties in the temperature range of 980–1050°C, making it particularly suitable for lightweight, integrated high-temperature components manufactured via additive manufacturing.
High corrosion resistance · Good creep resistance · Additive manufacturing
Process Advantages
High sphericity 95.88%: Plasma rotating electrode atomization technology, excellent sphericity, very few satellite balls, uniform and dense powder spreading
Hollow rate 0.01%: Plasma rotating electrode atomization technology, extremely few hollow powders, dense formed parts
Excellent corrosion resistance: outstanding corrosion resistance in both oxidizing and non-oxidizing environments, superior high-temperature strength, creep resistance, and oxidation resistance
Low oxygen and nitrogen content: oxygen content ≤85ppm, nitrogen content ≤100ppm, reducing the oxygen content of formed parts
Excellent powder performance: Good powder flowability (9.93/50g), narrow particle size distribution of 0-53μm powder (D10 is 29.23μm, D50 is 45.53μm, D90 is 69.34μm)
Powder Morphology
SEM image of CM247 powder prepared by PREP
LPBF prepared PREP CM247 sample
Print Performance
Application Scenario
Aircraft Engine Fuel Nozzle
Chemical Composition
Chemical composition Wt% of CM247 powder prepared by PREP