Inconel 718 printed by laser powder bed fusion is the nickel-chromium-iron superalloy built from fine gas-atomized powder, melted layer by layer under inert gas. Rapid solidification gives a fine cellular-dendritic structure with columnar grains along the build direction, so as-built properties differ between build orientations, and niobium segregates to cell boundaries. Parts carry high residual stress and a rough surface, so they need stress relief on the plate, support removal, solution and aging treatment, often hot isostatic pressing, and machining of critical surfaces. Typical uses are turbine and combustor components, heat exchangers, manifolds and ducts.
Compliance & Regulations
Each row is one condition this material was measured in. Its values and curves are in the tables and charts below, labelled with the condition; the ranges here span that row's own cited values and are never averaged across rows.
| Condition | Yield (MPa) | UTS (MPa) | Elongation (%) | E (GPa) | Density (kg/m³) | Values | Curves |
|---|---|---|---|---|---|---|---|
| Inconel 718 (SLM) | 810–889 | 960–1137 | 19.2 | — | — | 5 | 0 |
| Renishaw In718-0405 | — | — | — | — | 8190 | 4 | 0 |
14 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Elongation at Break(εf) | 8.700 – 51.50 | % | 125 entriesClick to expand | ||
Hardness (Brinell)(HB) | 466 | HB | EOS NickelAlloy IN718, heat-treated · EOS M 290 | 40 µm · heat-treated · DIN EN ISO 6506-1:2014 | ||
Hardness (Rockwell C)(HRC)2 entries | 47.00 | HRC | EOS NickelAlloy IN718, heat-treated · EOS M 290 | 40 µm · heat-treated · ISO 6508-1 | ||
| ↳ | 42.00 | HRC | Farsoon IN718, heat-treated · minimum · heat-treated · ISO6507-1 / ISO6508-1 | ||
Hardness (Vickers)(HV) | 265 – 488 | HV | 40 entriesClick to expand | ||
Reduction of Area(RA) | 31.50 – 52.50 | % | 6 entriesClick to expand | ||
Stress–Strain Curve(σ–ε) | — | Pa | 14 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS) | 0.7220 – 1.540 | GPa | 126 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 0.4860 – 1.380 | GPa | 126 entriesClick to expand | ||
Young's Modulus(E) | 131.0 – 219.0 | GPa | 36 entriesClick to expand | ||
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Melting Point / Solidus(Tm)2 entries | 1,570.7 range 1,533.2–1,608.2 | K | 3D Systems LaserForm Ni718 (A) | ||
| ↳ | 1,571.2 range 1,533.2–1,609.2 | K | Renishaw In718-0405 · Generic data - wrought material | ||
Thermal Conductivity(k)3 entries | 11.40 | W/(m·K) | 3D Systems LaserForm Ni718 (A) · 21°C | ||
| ↳ | 18.30 | W/(m·K) | 3D Systems LaserForm Ni718 (A) · 100°C | ||
| ↳ | 9.000 range 6.000–12.00 | W/(m·K) | Renishaw In718-0405 · Generic data - wrought material | ||
Coefficient of Thermal Expansion(α (CTE)) | 0.0000120 – 0.0000160 | 1/K | 10 entriesClick to expand | ||
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 8.150 – 8.250 | kg/m³ | 11 entriesClick to expand | ||
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data
| 3D Systems LaserForm Ni718 (A) | — | — | — | — | 8200 | 6 | 0 |
| Renishaw In718-0405, as-built | 636–758 | 943–1057 | 19.0–36.0 | 158–203 | — | 20 | 0 |
| Colibrium Additive Nickel 718, as-built | 620–810 | 970–1080 | 25.5–33.5 | 135–200 | — | 38 | 0 |
| 3D Systems LaserForm Ni718 (A), heat-treated | 1230–1380 | 1400–1540 | 12.0–23.0 | — | — | 6 | 0 |
| 3D Systems LaserForm Ni718 (A), as-built | 630–815 | 985–1100 | 23.0–36.0 | — | — | 6 | 0 |
| Colibrium Additive Nickel 718, HIP | 1100–1105 | 1350–1355 | 24.0–24.5 | 200–205 | — | 10 | 0 |
| Renishaw In718-0405, aged | 1202–1306 | 1391–1504 | 16.0–17.0 | 186–202 | — | 20 | 0 |
| Velo3D Inconel 718 | — | — | — | — | 8190 | 1 | 0 |
| EOS NickelAlloy IN718 | — | — | — | — | 8150–8250 | 14 | 0 |
| EOS NickelAlloy IN718, heat-treated | 1141–1270 | 1370–1531 | 12.0–20.0 | — | — | 48 | 0 |
| Farsoon IN718 | — | — | — | — | 8180 | 1 | 0 |
| Nikon SLM Solutions IN718, heat-treated | 925–985 | 1205–1290 | 11.0–24.0 | — | — | 14 | 0 |
| Renishaw In718-0405, HIP | 929–1088 | 1228–1379 | 17.0–25.0 | 201–219 | — | 20 | 0 |
| Colibrium Additive Nickel 718, aged | 1165–1315 | 1365–1495 | 15.0–18.5 | 173–201 | — | 37 | 0 |
| EOS NickelAlloy IN718, as-built | 620–800 | 957–1092 | 25.0–36.0 | — | — | 42 | 0 |
| Nikon SLM Solutions IN718, as-built | 520–785 | 880–1070 | 18.0–37.0 | — | — | 98 | 0 |
| Velo3D Inconel 718, HIP | 807–1103 | 1020–1350 | 11.3–24.2 | 131–207 | — | 72 | 0 |
| Farsoon IN718, heat-treated | 1050 | 1320 | 13.0 | — | — | 4 | 0 |
| as-built | 554–706 | 805–973 | 22.7–51.1 | — | — | 9 | 10 |
| solution treated 980 °C | 486–580 | 722–907 | 38.7–51.5 | — | — | 6 | 2 |
| solution treated + double aged | 1005–1234 | 1118–1398 | 8.7–18.9 | — | — | 6 | 2 |
Machines the manufacturer states for this material.