Inconel 718 Round Bar Suppliers & Stockist in India - ASTM B637 UNS N07718
ASTM B637 / ASME SB637 | UNS N07718 | AMS 5662 / 5663 | Sizes 3 mm to 600 mm
ASTM B637 / ASME SB637 | UNS N07718 | AMS 5662 / 5663 | Sizes 3 mm to 600 mm
Inconel 718 Round Bar (ASTM B637 / UNS N07718) is a precipitation-hardened nickel-chromium superalloy that achieves tensile strength above 1275 MPa in the aged condition — outperforming 316L stainless steel by a factor of 2.5x at room temperature and retaining over 80% of that strength at 650°C. Unifit Fastener stocks 3 mm to 600 mm diameters from its Mumbai warehouse with full AMS 5662 / AMS 5663 / NACE MR0175 certification and EN 10204 3.1 MTCs dispatched the same day.
Compliant with ASTM B637 and designated UNS N07718 (also known as Werkstoff 2.4668 or DIN 2.4668), this precipitation-hardenable alloy delivers an extraordinary combination of tensile strength, creep resistance, and oxidation resistance — even under continuous operating temperatures up to 700°C (1300°F). The secret to its exceptional strength lies in its unique metallurgical structure: the formation of a gamma double prime (γ″) phase through the interaction of niobium, nickel, and other trace elements. This phase, generated during the precipitation hardening heat treatment process, locks dislocations within the alloy matrix and dramatically boosts mechanical performance compared to conventionally processed nickel alloys.
We maintain a ready stock of Inconel 718 Round Bars in diameters ranging from 3 mm to 600 mm, covering all standard and custom lengths. Our bars conform to AMS 5662, AMS 5663, ASME SB 637, and NACE MR0175/ISO 15156, and are available in multiple surface finishes including bright, polished, rough turned, and centreless ground. Whether you are procuring bar stock for jet engine turbine discs, subsea wellhead packers, nuclear control rod mechanisms, or NACE MR0175-compliant downhole tooling, Unifit Fastener offers the technical expertise, full mill test certificates (MTC), and competitive pricing that Indian and global buyers demand.
| Other Trade Names | Alloy 718, Nickel Alloy 718, Inconel Alloy 718, Inconel 718 |
|---|---|
| UNS Number | N07718 |
| ASTM Standard | ASTM B637 |
| ASME Standard | ASME SB637 |
| AMS Specifications | AMS 5662, AMS 5663, AMS 5664 |
| DIN / Werkstoff | 2.4668 |
| NACE | NACE MR0175 / ISO 15156 |
| Round Bar Diameter Range | 3mm to 600mm |
| Length | 50mm to 6000mm or custom cut length |
| Hex Bar Range | 3mm to 180mm AF |
| Flat Bar Range | 0.5mm to 200mm thickness |
| Square Bar Range | 2mm to 200mm |
| Finish | Black, bright, peeled, polished, turned, ground, cold drawn |
| Supply Condition | Solution annealed, age hardened, precipitation hardened, forged, hot rolled |
| Density | 8.19 g/cm3 |
| Melting Range | 1260-1336°C |
| Maximum Service Temperature | Approximately 700°C |
| HS Classification | Nickel alloy bars and rods |
The following table lists the elemental composition of Inconel Alloy 718 in weight percentage, as defined by the ASTM B637 UNS N07718 standard:
| Element | Specification % | Typical % |
|---|---|---|
| Nickel + Cobalt (Ni + Co) | 50.00-55.00 | 52.00 |
| Chromium (Cr) | 17.00-21.00 | 19.00 |
| Iron (Fe) | Balance | 18.00 |
| Niobium + Tantalum (Cb + Ta) | 4.75-5.50 | 5.13 |
| Molybdenum (Mo) | 2.80-3.30 | 3.05 |
| Titanium (Ti) | 0.65-1.15 | 0.90 |
| Aluminium (Al) | 0.20-0.80 | 0.50 |
| Carbon (C) | 0.08 max | 0.04 |
| Manganese (Mn) | 0.35 max | 0.18 |
| Silicon (Si) | 0.35 max | 0.18 |
| Phosphorus (P) | 0.015 max | - |
| Sulfur (S) | 0.015 max | - |
| Cobalt (Co) | 1.00 max | - |
| Boron (B) | 0.006 max | - |
| Copper (Cu) | 0.30 max | - |
| Property | Minimum Value |
|---|---|
| 0.2% Proof Stress | 1034 MPa |
| Tensile Strength | 1275 MPa |
| Elongation | 12% |
| Hardness | 331 HB |
| Property | Minimum Value |
|---|---|
| 0.2% Proof Stress | 827 MPa |
| Tensile Strength | 1034 MPa |
| Elongation | 17% |
| Hardness | 40 HRC max |
| Condition | Yield Strength | Tensile Strength | Elongation | Reduction of Area |
|---|---|---|---|---|
| Solution treated and aged | 1034 MPa min | 1275 MPa min | 12% min | 15% min |
| NACE compliant condition | 827 MPa min | 1034 MPa min | 17% min | 25% min |
| Density | 8.19 g/cm3 |
|---|---|
| Melting Range | 1260-1336°C |
| Specific Heat | 435 J/kg-K |
| Thermal Conductivity | 11.4 W/m-K at 20°C |
| Electrical Resistivity | 1.25 micro-ohm-m |
| Modulus of Elasticity | 200 GPa |
| Coefficient of Expansion | 13.0 microm/m-°C |
| Magnetic Permeability | Slightly magnetic after heat treatment |
| Product Form | Size Range | Common Finish | Cutting Option |
|---|---|---|---|
| Round Bar | 3mm to 600mm dia | Black, bright, peeled, polished | Random length or cut length |
| Hex Bar | 3mm to 180mm AF | Bright, cold drawn, polished | Cut-to-size available |
| Flat Bar | 0.5mm to 200mm thickness | Hot rolled, machined, polished | Custom size available |
| Square Bar | 2mm to 200mm | Bright, black, polished | Custom length available |
| Forged Bar / Billet | As per project requirement | Forged and machined | Project cut size |
3mm, 4mm, 5mm, 6mm, 8mm, 10mm, 12mm, 16mm, 20mm, 25mm, 30mm, 32mm, 36mm, 40mm, 50mm, 60mm, 75mm, 80mm, 100mm, 120mm, 150mm, 200mm, 250mm, 300mm, 350mm, 400mm, 450mm, 500mm, and 600mm.
| Condition | Description | Typical Use |
|---|---|---|
| Solution Annealed | Heated and rapidly cooled to prepare for aging | General fabrication and machining |
| Precipitation Hardened | Aged to develop high strength | Aerospace, turbine, and high-load parts |
| AMS 5662 | Solution treated and aged bar | High strength aerospace applications |
| AMS 5663 | High-strength aged bar condition | Critical rotating and pressure components |
| NACE Condition | Controlled hardness and strength | Sour service and oilfield applications |
Inconel 718 is the alloy of choice wherever high strength at elevated temperatures, corrosion resistance, and dimensional stability are non-negotiable. Unifit Fastener supplies Inconel 718 bars to the following industries:
| Performance Property | Why It Matters |
|---|---|
| Outstanding High-Temperature Strength | Maintains tensile strength above 1000 MPa even at 650°C — ideal for jet engine and gas turbine components where other alloys fail. |
| Superior Corrosion & Oxidation Resistance | The passive chromium-oxide layer formed on the surface resists aggressive media including chlorides, sulfides, and high-temperature steam. |
| Excellent Weldability | Unlike many precipitation-hardenable alloys, Inconel 718 can be welded in both annealed and aged conditions without post-weld cracking. |
| Good Machinability | Can be machined in both annealed and aged states with the right tooling, cutting speeds (10-40 m/min), and feed rates. |
| Cryogenic Toughness | Retains ductility and impact resistance at temperatures as low as -196°C, making it viable for liquid nitrogen and LNG applications. |
| NACE / Sour-Gas Compliance | Meets NACE MR0175 / ISO 15156 for H2S service — critical for offshore and downhole oil & gas components. |
| Gamma Double Prime Strengthening | Unique γ″ strengthening phase (Ni3Nb) provides superior creep and stress-rupture resistance compared to gamma-prime alloys. |
| Property | Inconel 718 | Inconel 625 |
|---|---|---|
| Strengthening Mechanism | Precipitation hardening (γ″ phase) | Solid solution + carbide strengthening |
| Tensile Strength (room temp) | 130 ksi (900 MPa) typical | 100 ksi (690 MPa) typical |
| Yield Strength | 70 ksi (480 MPa) typical | 60 ksi (414 MPa) typical |
| Elongation | 25% min (in 2 in.) | 30% min (in 2 in.) |
| Max Service Temp | Up to 700°C (1300°F) | Up to 1093°C (2000°F) |
| Density | 8.19 g/cm3 (0.296 lb/in3) | 8.44 g/cm3 (0.305 lb/in3) |
| Thermal Conductivity | 9.6 BTU/hr·ft2·°F (16.7 W/m·K) | 6.8 BTU/hr·ft2·°F (11.9 W/m·K) |
| Primary Industry | Aerospace, oil & gas, nuclear | Marine, chemical, offshore |
| Weldability | Excellent (both conditions) | Outstanding (no cracking) |
| NACE Compliance | Yes — MR0175 / ISO 15156 | Yes — MR0175 / ISO 15156 |
| Standard | Country/Region | Designation |
|---|---|---|
| UNS | North America | N07718 |
| ASTM | United States | B637 |
| ASME | United States | SB-637 |
| AMS | United States | 5662 / 5663 / 5664 |
| JIS | Japan | NCF718 |
| DIN / W.-Nr. | Germany | 2.4668 |
| EN | Europe | NiCr19Fe19Nb5Mo3 |
| GOST* | Russia | KhN45MVTYuBR (Approx.) |
Note: Prices are indicative and subject to change based on current LME nickel rates, order quantity, heat treatment condition, and surface finish. Contact Unifit Fastener for the most current pricing.
| Description | Size / Quantity | Price (USD) | Price (GBP) |
|---|---|---|---|
| Alloy 718 Round Bar — 10 mm dia × 500 mm | 1 pc | Contact for Quote | ~£65 |
| Alloy 718 Round Bar — 10 mm dia × 500 mm | 2 pcs | Contact for Quote | ~£96 |
| Alloy 718 Round Bar — 10 mm dia × 2000 mm | 2 pcs | Contact for Quote | ~£202 |
| Alloy 718 Hex Bar — 10 mm (A/F) × 1000 mm | 1 pc | ~$101 | £101 |
| Alloy 718 Hex Bar — 10 mm (A/F) × 2000 mm | 3 pcs | ~$427 | £427 |
| OD 1.4" × 11" Long | 1 pc | $130.19 | — |
| 40 mm dia × 1.00 m Long | 1 pc | $512.02 | — |
| 60 mm dia × 1.00 m Long | 1 pc | $1,186.65 | — |
| 100 mm dia × 0.50 m Long | 1 pc | $1,661.67 | — |
Inconel 718 is a challenging alloy to machine due to its high work-hardening rate and elevated hot hardness. The following recommended cutting parameters help achieve optimal tool life and surface finish:
| Operation | Cutting Speed Vc (m/min) | Feed Rate f (mm/rev) | Notes |
|---|---|---|---|
| Rough Turning | 20-40 | 0.20-0.40 | Use carbide (K20-K30) or ceramic inserts |
| Finish Turning | 10-25 | 0.10-0.25 | Positive rake geometry; flood coolant |
| Drilling | 10-20 | 0.05-0.20 | High-speed steel or solid carbide; peck drill |
| Rough Milling | 15-30 | 0.05-0.15 mm/tooth | Avoid interrupted cuts where possible |
| Finish Milling | 10-20 | 0.03-0.10 mm/tooth | Maintain chip control; inspect inserts frequently |
Inconel 718 is a nickel-chromium-iron-niobium superalloy designated UNS N07718 (also Werkstoff Nr. 2.4668 under DIN and NCF 718 under JIS). Its primary alloying elements are nickel (50-55%), chromium (17-21%), iron (balance), and niobium+tantalum (4.75-5.50%), with controlled additions of molybdenum, titanium, and aluminum.
AMS 5662 covers Inconel 718 round bars in the solution-annealed condition (softened, ready for precipitation hardening by the end user), while AMS 5663 covers bars that are already solution-annealed AND precipitation-hardened (age-hardened) by the manufacturer. Buyers who intend to do their own heat treatment should specify AMS 5662; those needing ready-to-use maximum-strength bars should specify AMS 5663.
Inconel 718 retains adequate mechanical properties up to approximately 700°C (1300°F) under continuous service. Bright bar forms may operate intermittently up to 982°C (1800°F). Beyond these temperatures, other superalloys such as Inconel 625 or Hastelloy X are recommended.
Yes, Inconel 718 has excellent weldability in both annealed and age-hardened conditions — a significant advantage over many other precipitation-hardenable superalloys. Recommended welding processes include TIG (GTAW) and MIG (GMAW) using Inconel 718 filler wire (ERNiFeCr-2). To minimize heat-affected zone cracking, use low heat input, avoid large weld beads, and post-weld heat treat if required by the design code.
NACE MR0175 (ISO 15156) specifies material requirements for equipment used in oil and gas production environments containing hydrogen sulfide (H2S), commonly called sour service. Inconel 718 bars in the solution-annealed and aged condition with hardness not exceeding 40 HRC are qualified for sour-gas service under this standard. Unifit Fastener supplies NACE MR0175 compliant bars with full documentation.