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Inconel ® alloy 718
Precipitation hardenable alloy which gives corrosion resistance and high strength with excellent weldability. Excellent creep rupture strength at temperatures up to 700C. Uses include gas turbines, rocket motors, nuclear reactors and pumps.
Good strength/ductility properties from sub-zero temperatures to over 760°C
Excellent corrosion resistance and fatigue resistance in a wide variety of corrosive chemicals including seawater and industrial acids
Non-magnetic and spark resistant
Excellent resistance to stress corrosion cracking
Applications
Oil and Gas Industry:
Nuclear Power Plant:
Key Features:
Minimum Order Quantity: 1 Kg
Product Brochure
| Wire Gauge | 36 SWG |
| Type | Nickel Wire |
| Color | Silvery White |
| Application | Industry |
| Grade | Nickel Base Alloy |
| Powder Or Not | Not Powder |
Inconel 718, designated as UNS N07718 and Werkstoff Nr. 2.4668, is a nickel-chromium-iron superalloy that has gained worldwide acceptance for its exceptional mechanical strength, weldability, fatigue resistance, and corrosion resistance.
In its wire form, Inconel 718 becomes one of the most versatile materials for high-performance springs, fasteners, heating elements, aerospace components, and oilfield tools. The wire can be supplied in diameters ranging from 0.1 mm fine wire to several millimeters heavy wire depending on application needs.
Unlike many other superalloys that are difficult to weld or form, Inconel 718 wire offers excellent weldability, formability, and age-hardening capability, making it highly valuable in industries such as aerospace, defense, nuclear, oil & gas, marine, and medical.
Chemical Composition of Inconel 718 Wire
| Element | Content (%) |
|---|---|
| Nickel (Ni) | 50.0 – 55.0 |
| Chromium (Cr) | 17.0 – 21.0 |
| Iron (Fe) | Balance |
| Niobium (Nb) + Tantalum (Ta) | 4.75 – 5.50 |
| Molybdenum (Mo) | 2.80 – 3.30 |
| Titanium (Ti) | 0.65 – 1.15 |
| Aluminum (Al) | 0.20 – 0.80 |
| Cobalt (Co) | ≤ 1.0 |
| Manganese (Mn) | ≤ 0.35 |
| Silicon (Si) | ≤ 0.35 |
| Carbon (C) | ≤ 0.08 |
| Copper (Cu) | ≤ 0.30 |
| Boron (B) | ≤ 0.006 |
Tensile Strength: ~1375 MPa
Yield Strength (0.2%): ~1035 MPa
Elongation: 12–20%
Hardness: ~363 HB
Excellent fatigue resistance
Creep rupture strength maintained up to 650 °C
Density: 8.19 g/cm³
Melting Range: 1260 – 1336 °C
Elastic Modulus: 200 GPa
Thermal Conductivity: 11.4 W/m·K
Specific Heat: 435 J/kg·K
Electrical Resistivity: 125 μΩ·cm
Magnetic Properties: Non-magnetic (annealed)
Tensile Testing: Ensures strength.
Bend Test: For spring wires.
Corrosion Testing: For marine and chemical uses.
NDT: Eddy current and ultrasonic inspection.
Dimensional Check: Diameter tolerance per ASTM/AMS.
Additional Information:
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Minimum Order Quantity: 10 Kilogram
Product Brochure
| Thickness | 6 mm |
| Grade | 718 |
| Shape | Rectangle |
| Material | Steel |
| Usage/Application | Industry |
| Application | Industrial |
Inconel 718, designated as UNS N07718, is a high-strength, corrosion-resistant nickel-chromium alloy that is extensively used in environments exposed to extreme temperatures, pressure, and aggressive corrosion. When manufactured in sheet form, it is widely employed in aerospace structures, gas turbines, chemical processing equipment, nuclear reactors, and marine applications.
The sheet form of this alloy offers superior formability, fatigue resistance, and creep strength, which makes it ideal for components that require precision fabrication and long service life in high-stress environments.
Chemical CompositionThe chemical composition of Inconel 718 is carefully engineered to balance mechanical performance and corrosion resistance:
| Element | Percentage (%) |
|---|---|
| Nickel (Ni) | 50.0 – 55.0 |
| Chromium (Cr) | 17.0 – 21.0 |
| Iron (Fe) | Balance |
| Niobium (Nb) + Tantalum (Ta) | 4.75 – 5.50 |
| Molybdenum (Mo) | 2.80 – 3.30 |
| Titanium (Ti) | 0.65 – 1.15 |
| Aluminum (Al) | 0.20 – 0.80 |
| Cobalt (Co) | ≤ 1.0 |
| Carbon (C) | ≤ 0.08 |
| Manganese (Mn) | ≤ 0.35 |
| Phosphorus (P) | ≤ 0.015 |
| Sulfur (S) | ≤ 0.015 |
| Silicon (Si) | ≤ 0.35 |
| Copper (Cu) | ≤ 0.30 |
| Boron (B) | ≤ 0.006 |
One of the defining strengths of Inconel 718 sheets is their impressive mechanical profile, especially under high temperatures and long-term loads:
| Property | Value |
|---|---|
| Tensile Strength | Up to 1380 MPa |
| Yield Strength | Up to 1100 MPa |
| Elongation | ~12–23% |
| Hardness (Rockwell C) | 33–45 HRC |
| Operating Temperature Range | −250°C to 704°C |
| Creep Rupture Strength | Excellent |
| Fatigue Resistance | Outstanding |
Inconel 718 achieves its strength through precipitation hardening via the formation of γ'' (gamma double prime – Ni3Nb) and γ' (gamma prime – Ni3(Al, Ti)) phases.
Specifications and StandardsInconel 718 Sheets must comply with several international specifications for quality and traceability:
| Standard | Description |
|---|---|
| ASTM B670 | Standard Specification for Nickel-Chromium-Iron Alloy (UNS N07718) Sheet, Strip, and Plate |
| AMS 5596 | Aerospace Specification for Sheet and Strip |
| ASME SB-670 | Boiler and Pressure Vessel Code |
| ISO 15156 / NACE MR0175 | For use in H₂S-containing environments in oil and gas production |
0.8 mm, 1 mm, 2 mm, 3 mm, 4 mm, 5 mm
Additional Information:
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Minimum Order Quantity: 10 Kg
Product Brochure
| Length | 6 meter |
| Grade | 718 |
| Shape | Round |
| Brand | IMPORTED |
| Type | Bar |
| Material Grade | INCONEL 718 |
| Single Piece Length | 3 meter, 6 meter |
| Size | 0.1MM - 500MM |
| Usage/Application | Industrial |
| Material | Inconel 718 |
Inconel 718 (UNS N07718 / W.Nr. 2.4668) is a nickel-chromium superalloy that has earned global recognition for its exceptional combination of high strength, corrosion resistance, and remarkable weldability. Unlike many other nickel alloys, Inconel 718 maintains outstanding performance from cryogenic temperatures up to about 704 °C (1300 °F).
The round bar form of Inconel 718 is widely used in industries such as aerospace, oil & gas, marine, chemical processing, and nuclear engineering, where both mechanical reliability and corrosion resistance are critical. Its ability to resist creep, stress rupture, fatigue, and oxidation makes it ideal for rotating parts, fasteners, shafts, and components exposed to extreme thermal and mechanical loads.
Chemical Composition of Inconel 718 Round Bar
| Element | Percentage (%) |
|---|---|
| Nickel (Ni) | 50.0 – 55.0 |
| Chromium (Cr) | 17.0 – 21.0 |
| Iron (Fe) | Balance |
| Niobium (Nb) + Tantalum (Ta) | 4.75 – 5.50 |
| Molybdenum (Mo) | 2.80 – 3.30 |
| Titanium (Ti) | 0.65 – 1.15 |
| Aluminum (Al) | 0.20 – 0.80 |
| Cobalt (Co) | ≤ 1.0 |
| Manganese (Mn) | ≤ 0.35 |
| Silicon (Si) | ≤ 0.35 |
| Carbon (C) | ≤ 0.08 |
| Copper (Cu) | ≤ 0.30 |
| Boron (B) | ≤ 0.006 |
Tensile Strength: ~1375 MPa
Yield Strength (0.2% offset): ~1035 MPa
Elongation: ~12 – 20%
Hardness: ~363 HB
Fatigue Strength: Excellent under cyclic loads
Creep-Rupture Strength: Outstanding up to 650 °C
Density: 8.19 g/cm³
Melting Range: 1260 – 1336 °C
Elastic Modulus: ~200 GPa
Thermal Conductivity: 11.4 W/m·K at 100 °C
Specific Heat: 435 J/kg·K
Electrical Resistivity: 125 μΩ·cm
Magnetic: Non-magnetic in annealed condition
Mechanical Testing: Tensile, impact, hardness.
Corrosion Tests: Pitting and crevice testing.
NDT: Ultrasonic, Eddy current, MPI.
Dimensional Accuracy: Tolerances per ASTM/ASME.
Microstructural Analysis: To ensure correct γ′/γ″ precipitation.
Additional Information:
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Minimum Order Quantity: 10 Kilogram
Product Brochure
| Type | Plate |
| Grade | 718 |
| Usage/Application | Chemical Handling |
| Plate Type | Inconel Plate |
Inconel 718, also known by its UNS designation N07718 and Werkstoff Nr. 2.4668, is one of the most widely used nickel-chromium superalloys in demanding engineering applications. Developed in the 1960s, it became a cornerstone alloy for aerospace engines, gas turbines, oil & gas equipment, and chemical process plants due to its unique balance of high strength, corrosion resistance, weldability, and fatigue performance.
In its plate form, Inconel 718 offers engineers a versatile material that can be cut, machined, formed, and fabricated into critical components such as heat shields, turbine casings, structural panels, and pressure vessel plates. Unlike some superalloys, Inconel 718 combines excellent mechanical strength with good fabrication properties, making it the preferred material for both high-temperature and cryogenic applications.
Chemical Composition of Inconel 718 Plate
| Element | Content (%) |
|---|---|
| Nickel (Ni) | 50.0 – 55.0 |
| Chromium (Cr) | 17.0 – 21.0 |
| Iron (Fe) | Balance |
| Niobium (Nb) + Tantalum (Ta) | 4.75 – 5.50 |
| Molybdenum (Mo) | 2.80 – 3.30 |
| Titanium (Ti) | 0.65 – 1.15 |
| Aluminum (Al) | 0.20 – 0.80 |
| Cobalt (Co) | ≤ 1.0 |
| Manganese (Mn) | ≤ 0.35 |
| Silicon (Si) | ≤ 0.35 |
| Carbon (C) | ≤ 0.08 |
| Copper (Cu) | ≤ 0.30 |
| Boron (B) | ≤ 0.006 |
Tensile Strength: ~1375 MPa
Yield Strength (0.2%): ~1035 MPa
Elongation: 12–20%
Hardness: ~363 HB
Creep-Rupture Strength: Excellent up to 650 °C
Fatigue Life: Very high under cyclic stresses
Density: 8.19 g/cm³
Melting Range: 1260 – 1336 °C
Elastic Modulus: 200 GPa
Thermal Conductivity: 11.4 W/m·K at 100 °C
Specific Heat: 435 J/kg·K
Electrical Resistivity: 125 μΩ·cm
Magnetic Behavior: Non-magnetic (annealed condition)
The strength of Inconel 718 plate is derived from precipitation hardening involving two primary phases:
γ′ (Ni₃(Al,Ti)) → enhances strength.
γ″ (Ni₃Nb) → main hardening phase unique to Inconel 718.
Chemical Analysis: Spectrographic and wet analysis.
Mechanical Testing: Tensile, hardness, impact tests.
Corrosion Testing: Pitting, crevice, intergranular corrosion.
NDT: Ultrasonic, radiographic, eddy current inspection.
Dimensional Tolerance: Per ASTM B670 and AMS standards.
Additional Information:
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