Related Specifications
Surface Treatments
Certifications
- ISO 9001 - 2015 Certified
- PED 2014/68/EC
- NACE MR0175/ISO 15156-2
- NORSOK M-650
- DFAR
- MERKBLATT AD 2000 W2/W7/W10
Inconel 718 / Alloy 718 / W.Nr 2.4668 / Nickel-Chromium-Niobium Precipitation-Hardening Superalloy
UNS N07718 is the Unified Numbering System designator for the precipitation-hardening nickel-chromium-niobium superalloy commercially branded Inconel 718 by Special Metals and Alloy 718 by other producers. In Europe the equivalent designator is Werkstoff Nr. 2.4668. The same alloy is the subject of ASTM A1014 for bolting components, ASTM B637 for bar and forging stock, SAE AMS 5662 (solution heat treated) and AMS 5663 (solution + precipitation hardened) for aerospace procurement, and ASME PVP Code Case 1993-7 for pressure-vessel service.
UNS N07718 sits in the SAE/ASTM Unified Numbering System under the "N" prefix for nickel and nickel alloys. The five-digit code identifies a single specific nickel-chromium-niobium chemistry developed in the 1960s by INCO (now Special Metals) for high-temperature aerospace bolting, gas-turbine compressor discs, and oilfield downhole tools. The alloy strengthens through precipitation of γ″ (gamma double-prime, Ni₃Nb) and γ′ (gamma prime, Ni₃(Al,Ti)) phases during age hardening, giving 185 ksi tensile strength at room temperature that retains 145 ksi at 1200 °F (650 °C).
| Element | Composition (mass %) |
|---|---|
| Nickel + Cobalt | 50.0 – 55.0 |
| Chromium | 17.0 – 21.0 |
| Molybdenum | 2.80 – 3.30 |
| Niobium + Tantalum | 4.75 – 5.50 |
| Titanium | 0.65 – 1.15 |
| Aluminum | 0.20 – 0.80 |
| Cobalt, max | 1.0 |
| Carbon, max | 0.08 |
| Iron | Remainder |
Niobium content is the discriminating element: it pushes UNS N07718 into the γ″-strengthened family vs UNS N06625 (Inconel 625) which is primarily solid-solution strengthened. The deliberately slow γ″ precipitation kinetics give UNS N07718 the best weldability of any precipitation-hardening superalloy.
| Property | Room Temperature | 1200 °F (650 °C) |
|---|---|---|
| Tensile strength, min | 185 ksi (1275 MPa) | 145 ksi (1000 MPa) |
| 0.2% yield strength, min | 150 ksi (1035 MPa) | 125 ksi (860 MPa) |
| Elongation, min | 12 % | 12 % |
| Reduction of area, min | 15 % | 15 % |
| Brinell hardness | 331 – 444 HBW | - |
| Stress rupture (100 ksi) | - | 23 hours minimum |
| Standard | Product Form / Scope |
|---|---|
| ASTM A1014 / A1014M | Bolting components: bolts, studs, screws (this site) |
| ASTM B637 | Bar, forgings, and forging stock for elevated-temperature service |
| SAE AMS 5662 | Aerospace bar & forging, solution heat treated |
| SAE AMS 5663 | Aerospace bar & forging, solution + age hardened (final bolt condition) |
| SAE AMS 5664 | Aerospace bar & forging, higher-strength solution + age hardened |
| SAE AMS 5596 | Sheet, strip, and plate, solution treated |
| SAE AMS 5597 | Sheet, strip, and plate, age hardened |
| SAE AS 7467 | Aerospace bolts / screws, 185 ksi tensile, stress-rupture rated |
| MS14181 / AS3418 / NAS1351 | Mil-Spec aerospace bolt part numbers in UNS N07718 |
| ASME PVP Code Case 1993-7 | Pressure-vessel code case authorizing UNS N07718 bolting |
For finished bolting in UNS N07718 / Inconel 718, browse the ASME B18 dimensional families covered on this site: