Alloy 625 is a nickel-chromium alloy which gains its stiffening effect through molybdenum and niobium additions, therefore eliminating the need for this alloy to be aged. It has superior resistance to a wide range of corrosive environments as well as the high temperature effects of oxidation and carburisation.
This alloy also has high tensile, creep and rupture strength, fatigue and thermal fatigue strength and oxidation resistance, making it suitable for aircraft engine exhaust systems, housing engine controls and aircraft ducting systems. It is also used in the nuclear field for reactor cores, control rod components in nuclear water reactors.
| C | Mn | Si | P | S | Cr | Ni | Co | Ti | Ai | Mo | Nb + Ta | Fe | - | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Min | - | - | - | - | - | 20.0 | 58.0 | - | - | - | 8.0 | 3.15 | - | % |
| Max | 0.10 | 0.50 | 0.50 | 0.15 | 0.15 | 23.0 | - | 1.0 | 0.40 | 0.40 | 10.0 | 4.15 | 5.0 | % |
Typical properties for Annealed Grade 1 up to 100mm section:
| Tensile (PSI (MPA)) | Yield (0.2% offset), (PSI (MPA) Min) | Elongation in 2" or 4D min% | Reduction of Area | Rockwell Hardness HRC Max | Charpy Impacts at - 70◦C Joules (ftlb) min |
|---|---|---|---|---|---|
| 120,000(827) | 60,000(413) | 30 | 35 | 35 | Average 42 (31) Single 33(25) |
Our products are inspected rigorously for a variety of quality attributes to ensure they arrive in perfect condition and without errors.
Proven aility to execute small and large batch orders with an unwavering commitment to on-time delivery.
