| Customization: | Available |
|---|---|
| Application: | Aviation, Electronics, Industrial, Medical, Chemical |
| Standard: | JIS, GB, DIN, BS, ASTM, AISI |
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NIMONIC 80A
A nickel-chromium alloy similar to NIMONIC alloy 75 but made precipitation hardenable by additions of aluminum and titanium. The alloy has good corrosion and oxidation resistance and high tensile and creep-rupture properties at temperatures to 1500ºF(815ºC). Used for gas-turbine components (blades, rings, and discs), bolts, tube supports in nuclear steam generators, die-casting inserts and cores, and exhaust valves in internal-combustion engines.
Nimonic 80A Chemaical composition:
| Alloy | % | Ni | Cr | Fe | Mn | Si | P | S | Al | Ti | C | Co | B | Zr | Cu |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 625 | Min. | Balance | 18 | 1.0 | 1.8 | ||||||||||
| Max. | 21 | 3.0 | 1.0 | 1.0 | 0.02 | 0.015 | 1.8 | 2.7 | 0.1 | 2.0 | 0.008 | 0.15 | 0.2 |
Nimonic 80A Physical properties:
| Density | 8.19 g/cm3 |
| Melting range | 1320-1365ºC |
Nimonic 80A minimum mechanical properties in the room temperature:
| Status | Tensile strength Rm N/mm2 |
Yield strength RP0.2N/mm2 | Elongation A5 % |
| Nimonic 80A | 930 | 620 | 20 |
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