Material Characteristics
IN625 is a nickel-chromium-molybdenum-niobium alloy that exhibits excellent corrosion resistance to a variety of corrosive media. It combines high strength, excellent weldability and excellent creep rupture strength up to 700 °C. For example, Inconel 625 is used in aircraft engines and heat exchangers.
| Properties | Unit | As built 1) | Heat-treated 2) |
|---|---|---|---|
| Tensile Strength Rm | Mpa | 1020 ±30 | 1030 ±30 |
| Yield Strength Rp0,2 | MPa | 700 ±30 | 660 ±20 |
| Elongation at Break A5 | % | 37 ±5 | 40 ±5 |
| Young‘s Modulus E | GPa | 180 ±10 | 195 ±10 |
| Hardness | HV | 290 ±5 | 285 ±5 |
- The specified material properties were determined at room temperature. They are multidimensionally dependent on many different machine and process parameters. Without further investigation, the material properties do not constitute a sufficient basis for component dimensioning.
- Specific heat treatment processes lead to optimized mechanical-technological properties to meet the component requirements.
Rosswag Engineering offers a holistic and fully integrated process chain for Additive Manufacturing services. Our portfolio ranges from manufacturing of your prototypes, tools and small serial products to an individual consulting and engineering process for the choice of material, parameters and process chain.
+49 7240 9410-131
info@rosswag-engineering.de
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