Ni-based superalloys Osprey® Alloy 625 and Alloy 718 are produced using an vacuum induction melting process. This results in powders with significantly lower oxygen and nitrogen levels than conventional metallurgy, typically below 250 ppm. Lower levels of O and N can be offered but needs to be discussed related to the type of Ni-based alloy.
Material properties
Typical material properties of Osprey® Alloy 625 and Alloy 718, melted under vacuum.
Osprey® Alloy 625
Material properties
- Attractive mechanical strength in combination with excellent corrosion resistance, particularly good resistance to marine corrosion
- Performs well in ambient to elevated temperatures up to ~815°C related to rupture resistance, creep resistance, and resistance to corrosive attacks
Additive processes
- Powder Bed Fusion, Laser
- Powder Bed Fusion, Electron Beam
Typical uses/Applications
- Critical corrosion resistant components
- Pressure vessels
- Chemical processing components
Powder bed fusion – Laser (as built) |
Properties for Osprey® Alloy 625 nickel-based superalloy
Parameter |
Vertical Direction |
ASTM F3056 14a |
Horizontal Direction |
Yield Strength [MPa] |
690 |
275 |
825 |
Tensile Strength [MPa] |
980 |
485 |
1100 |
Elongation (%) |
44 |
30 |
33 |
Impact toughness [J] |
186 |
- |
122 |
Powder bed fusion – Electron beam (as built) |
Parameter |
Vertical Direction |
ASTM F3056 14a |
Horizontal Direction |
Yield Strength [MPa] |
390 |
275 |
360 |
Tensile Strength [MPa] |
840 |
485 |
750 |
Elongation (%) |
39 |
30 |
33 |
Impact toughness [J] |
98 |
- |
46 |
Osprey® Alloy 718
Material properties
- High mechanical strength in combination with high corrosion resistance
- Attractive mechanical properties at elevated temperatures up to ~650°C
Additive processes
- Powder Bed Fusion, Laser
- Powder Bed Fusion, Electron Beam
Typical uses/Applications
- Jet turbines
- Gas turbines
- Oil and gas
Powder bed fusion – Laser (as built) |
Properties for Osprey® Alloy 718 nickel-based superalloy
Parameter |
Vertical Direction |
ASTM F3055 14 |
Horizontal Direction |
Yield Strength [MPa] |
660 |
600 |
790 |
Tensile Strength [MPa] |
930 |
920 |
1040 |
Elongation (%) |
61 |
27 |
50 |
Impact toughness [J] |
108 |
- |
- |
Powder bed fusion – Electron beam (as built) |
Parameter |
Vertical Direction |
ASTM F3055 14 |
Horizontal Direction |
Yield Strength [MPa] |
980 |
600 |
860 |
Tensile Strength [MPa] |
1210 |
920 |
1070 |
Elongation (%) |
19 |
27 |
29 |
Impact toughness [J] |
20 |
- |
20 |
Osprey® Alloy H-X
Material properties
- Attractive mechanical strength in combination with excellent corrosion resistance, stress corrosion cracking, oxidation resistance and high-temperature strength
- Performs well in ambient with good ductility after exposure to elevated temperatures up to ~870°C
Additive processes
- Powder Bed Fusion, Laser
- Powder Bed Fusion, Electron Beam
- Binder Jet
- Direct Energy Deposition & Laser Cladding
Typical uses/Applications
- Gas turbine engines, including combustor cans & after-burners
- Furnace rolls & baffles
- Critical corrosion resistant components
Powder bed fusion – Laser (as built) |
Properties for Osprey® Alloy H-X nickel-based superalloy
Parameter |
Vertical Direction |
|
Horizontal Direction |
Yield Strength [MPa] |
522 |
|
627 |
Tensile Strength [MPa] |
684 |
|
820 |
Elongation (%) |
41 |
|
31 |
Impact toughness [J] |
156 |
|
105 |
Powder bed fusion – Laser (heat treated) |
Parameter |
Vertical Direction |
Plate, solution heat treated |
Horizontal Direction |
Yield Strength [MPa] |
390 |
324 |
444 |
Tensile Strength [MPa] |
637 |
721 |
770 |
Elongation (%) |
52 |
46 |
40 |
Impact toughness [J] |
194 |
140 |
156 |
Powder bed fusion – Laser (heat treated) and tested at 815°C |
Parameter |
Vertical Direction |
Plate, solution heat treated |
Horizontal Direction |
Yield Strength [MPa] |
169 |
~200 |
|
Tensile Strength [MPa] |
292 |
~300 |
|
Elongation (%) |
21 |
~80 |
|
Impact toughness [J] |
|
|
|
Material datasheets
Other Ni-based superalloys are also available. View the range of alloys