Inconel 718 is a precipitation-hardenable nickel-chromium superalloy that delivers exceptional strength from -423°F (-253°C) up to 1300°F (700°C). Its unique combination of high tensile strength, fatigue resistance, creep rupture properties, and excellent weldability sets it apart from other high-strength superalloys.
Unlike many precipitation-hardened alloys that are prone to post-weld cracking, Inconel 718 exhibits outstanding weldability - even in complex, thin-walled fabrications. This makes it the #1 choice for aerospace gas turbine engines, liquid-fueled rockets, high-temperature fasteners, and critical oil & gas downhole components.
The unique age-hardenable characteristics come from a precise balance of niobium (columbium), titanium, and aluminum, which form strengthening precipitates (gamma double-prime and gamma prime) during heat treatment.
| Element | Content (%) | Role |
|---|---|---|
| Nickel (Ni) | 50.0 - 55.0 | Base element - provides corrosion resistance & austenitic stability |
| Chromium (Cr) | 17.0 - 21.0 | Oxidation resistance & protection against sulfur compounds |
| Iron (Fe) | Balance (Rem) | Provides cost-effective stability & structural integrity |
| Niobium + Tantalum (Nb+Ta) | 4.75 - 5.50 | Primary strengthening element (gamma double-prime precipitate) |
| Molybdenum (Mo) | 2.80 - 3.30 | Pitting resistance & solid-solution strengthening |
| Titanium (Ti) | 0.65 - 1.15 | Secondary strengthener (gamma prime precipitate) |
| Aluminum (Al) | 0.20 - 0.80 | Secondary strengthener (gamma prime precipitate) |
| Cobalt (Co) | 1.00 max | Limited for nuclear compatibility |
| Carbon (C) | 0.08 max | Controlled for carbide stability |
| Manganese (Mn) | 0.35 max | Trace element |
| Silicon (Si) | 0.35 max | Trace element |
| Phosphorus (P) | 0.015 max | Controlled for ductility |
| Sulfur (S) | 0.015 max | Controlled for hot workability |
| Boron (B) | 0.006 max | Grain boundary strengthener |
| Copper (Cu) | 0.30 max | Trace element |
Inconel 718 is supplied in two main conditions: Solution Annealed (for fabrication) and Aged (precipitation-hardened for maximum strength). The aged condition delivers the alloy's signature high-temperature performance.
| Product Form | Condition | Tensile Strength (KSI / MPa) | Yield Strength 0.2% Offset (KSI / MPa) | Elongation (%) | Hardness |
|---|---|---|---|---|---|
| Sheet (AMS 5596) | Solution Annealed | 140 KSI (965 MPa) | 80 KSI (552 MPa) | 30 | 102 HRB max |
| Sheet (AMS 5596) | Aged | 180 KSI (1241 MPa) | 150 KSI (1034 MPa) | 12 | ≥36 HRC |
| Sheet (AMS 5597) | Solution Annealed | 140 KSI (965 MPa) | 75 KSI (517 MPa) | 30 | ≤25 HRC |
| Sheet (AMS 5597) | Aged | 180 KSI (1241 MPa) | 150 KSI (1034 MPa) | 15 | ≥38 HRC |
| Bar / Rod (ASTM B637) | Solution Annealed + Aged | 185 KSI min (1276 MPa) | 150 KSI min (1034 MPa) | 12 min | 36 HRC min |
We supply Inconel 718 in all standard mill forms, cut to size, with full traceability to AMS, ASTM, and ASME standards. Custom dimensions and special heat treatments are available upon request.
| Product Form | Size Range | Key Specifications |
|---|---|---|
| Round Bar / Rod | Dia: 6mm - 300mm (0.25" - 12") | ASTM B637, ASME SB637, AMS 5662, AMS 5663, AMS 5664, ISO 9723, DIN 17752 |
| Wire | Dia: 0.1mm - 12mm | AMS 5832, ISO 9724, DIN 17753 |
| Plate / Sheet / Strip | Thk: 0.5mm - 100mm | ASTM B670, ASTM B906, AMS 5596, AMS 5597, AMS 5598, AMS 5862, ISO 6208, DIN 17750 |
| Seamless Pipe / Tube | OD: 6mm - 219mm | SAE AMS 5589, SAE AMS 5590, ASTM B983 |
| Welded Pipe / Tube | OD: up to 914mm | SAE AMS 5590 (welded annealed), ASTM B983 |
| Fittings (Flanges, Elbows, Tees) | All schedules | ASTM B366, ASME SB366 |
| Forgings (Rings, Discs, Blocks) | Custom sizes | ASTM B637, ASME SB637, AMS 5663, ISO 9725, DIN 17754 |
| Fastener Stock | Custom | ASTM B637 (Condition A or Aged), AMS 5662 |
Need Inconel 718 bar, sheet, pipe, or custom forgings for high-temperature, high-stress applications?