Alloy 80A
About Alloy 80A
What is Alloy 80A?
Alloy 80A also referred to as the UNS N07080/W.Nr. 2.4952 alloy.
It is a wrought, age-hardenable nickel-chromium alloy, strengthened by additions of titanium, aluminum and carbon, developed for service at temperatures up to 815°C (1500°F)
Alloy 80A is widely used in gas turbine components (blades, rings and discs), bolts, nuclear boiler tube supports, die casting inserts and cores, and automobile exhaust valves.
Alloy 80A is available in the form of sheet, round bar, flat bar, forging, hexagon, wire, plate and extruded section.
Alloy 80A Standards
BS HR 401
-Seamless Pipe & Tube
BS HR 201
-Plate, Sheet, Strip & Foil
Alloy 80A Chemical Composition
Alloy 80A Data Sheet
Alloy 80A Equivalent Grades
| STANDARD | WERKSTOFF NR. | UNS | GOST | AFNOR | JIS | BS | EN | OR |
| Alloy 80A | 2.4952/2.4631 | N07080 | – | – | – | – | – | – |
Alloy 80A Mechanical Properties
| Density | Melting Point | Tensile Strength | Yield Strength (0.2%Offset) | Elongation |
| 8.19 g/cm3 | 1365°C (2490°F) | 1250Mpa | 780Mpa | 30% |
Alloy 80A Applications
Alloy 80A Related Resources
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