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Atomfair GH4099 Nickel-Based Superalloy Powder (SLM Grade)
GH4099 is a Ni-based precipitation-hardened superalloy, suitable for long-term service below 900°C and short-term use up to 1000°C. It exhibits excellent thermal strength and good hot/cold work formability, making it ideal for high-temperature welded structural components like aero-engine combustion chambers and afterburners. Compatible with the SLM process.
Description
Chemical Composition (wt.%) | |
---|---|
Ni | Balance |
Cr | 17.0-20.0 |
Co | 5.0-8.0 |
Mo | 5.0-7.0 |
Al | 3.5-4.5 |
Ti | 1.7-2.4 |
C | ≤0.08 |
Mg | ≤0.01 |
Ce | ≤0.02 |
B | ≤0.005 |
Fe | ≤2.0 |
P | ≤0.015 |
S | ≤0.015 |
Mn | ≤0.4 |
Si | ≤0.5 |
O | ≤0.02 |
N | ≤0.02 |
Physical Properties | |
---|---|
Particle Size (μm) | D10≥15, D50:30-40, D90≤58 |
Sphericity | ≥0.9 |
Apparent Density (g/cm³) | ≥4.4 |
Tapped Density (g/cm³) | ≥5.0 |
Flowability (s/50g) | ≤18 |
Mechanical Properties (Heat Treated) | |||
---|---|---|---|
Condition | Tensile Strength (MPa) | Yield Strength (MPa) | Elongation (%) |
Room Temp | ≥1000 | ≥600 | ≥35.0 |
900°C | ≥400 | ≥350 | ≥15.0 |
Precipitation-hardened nickel-based superalloy for long-term service below 900°C (short-term up to 1000°C). Excellent thermal strength and formability. Typical applications include aero-engine combustion chambers and afterburner components.