EOS NickelAlloy 247
Material Data Sheet
EOS NickelAlloy 247
EOS NickelAlloy 247 is a high gamma prime fraction Ni-base superalloy with a combination of strength and oxidation resistance at elevated temperature.
EOS NickelAlloy 247 requires advanced processing and post-processing/heat treatment strategies for successful component fabrication, which are offered in combination with EOS consulting and application development by AdditiveMinds.
High strength at elevated temperatures
Creep resistance
Oxidation and hot corrosion resistance
Gas turbine hot gas path components; nozzle guide vanes, blades, ring segments
Integrally bladed disks (blisks) turbopump rotors
Engineering components for sustained service at elevated temperatures
The EOS Quality Triangle
EOS incorporates these TRLs into the following two categories:
- Premium products (TRL 7-9): offer highly validated data, proven capability and reproducible part properties.
- Core products (TRL 3 and 5): enable early customer access to newest technology still under development and are therefore less mature with less data.
All of the data stated in this material data sheet is produced according to EOS Quality Management System and international standards
POWDER PROPERTIES
EOS NickelAlloy 247 powder composition matches the composition of cast versions of the same superalloy. The powder is manufactured by vacuum inert gas atomization and gas atomization. Impurities and tramp elements are strictly controlled.
Powder Chemical Composition (wt.-%)
| Element | Min. | Max. |
|---|---|---|
| Ni | Balance | |
| W | 9 | 10 |
| Co | 8.8 | 9.6 |
| Cr | 7.7 | 8.5 |
| Al | 5.4 | 5.8 |
| Ta | 3 | 3.4 |
| Hf | 1.2 | 1.6 |
| Mo | 0.4 | 0.6 |
| C | 0.07 | 0.09 |
| B | 0.01 | 0.02 |
| Zr | 0.005 | 0.015 |
| Fe | - | 0.15 |
| Si | - | 0.15 |
| Mn | - | 0.01 |
| Nb | - | 0.1 |
| V | - | 0.1 |
| Cu | - | 0.01 |
| Mg | - | 0.006 |
Powder Particle Size
| GENERIC PARTICLE SIZE DISTRIBUTION | 20 - 53 μm | |
|---|---|---|
HEAT TREATMENT
EOS NickelAlloy 247 requires careful selection of heat treatment, which can beoptimized for the specific component to be manufactured and its functional requirements.
Heat treatment typically includes a stress relief and solution treatment (this may be done within a HIP) followed by an ageing heat treatment.
Shot peening is recommended prior to heat treatment.