NickelAlloy IN718
Description
This kind of precipita- tion-hardening nickel-chromium alloy is charac terized by having good tensile, fatigue, creep and rupture strength at temperat ures up to 700 °C (1290 °F). This material is ideal for many high temperature applications such as gas turbine parts, instru- mentation parts, power and process industry pa rts etc. It also has excellent potential for cryogenic applications.
Additional information
Specification: NickelAlloy IN718
| Header | NickelAlloy IN718 |
|---|---|
| Model number | NickelAlloy IN718 |
| Brand | EOS |
| Material name | NickelAlloy IN718 |
| Technology | DMLS / SLM |
| How it comes | Metal Powder |
| General material type | Metal |
| Material group specific material type | Nickel |
| Colour | Metallic |
| Datasheet | https://dl.airtable.com/dTbbllmsTjC09Xz9G4WT_EOS_NickelAlloy_IN718_en.pdf |
| Tensile strength ultimate xy in mpa | 1241 |
| Tensile strength yield xy in mpa | 1034 |
| Elongation at break xy | 12 |
| Modulus of elasticity xy in mpa | 170 |
| Rockwell hardness hrc | 47 |
| Brinell hardness hb | 446 HB |
| Density g cm | 8.15 |
| Legal disclaimer | 3DC LTD is not liable for the accuracy of the information contained within this database. Please consult directly with the relevant machine and/or material manufacturers before determining fitness for a particular use. |
