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Inconel 718, Alloy 718, 2.4668, N07718

Grade

Code

UNS

Nickel Alloys

Inconel 718

Alloy 718 (2.4668)

N07718

 

Nickel Alloy Properties

 

Inconel 718 / Alloy 718 is a precipitation-hardenable nickel-chromium-based superalloy containing significant amounts of iron, niobium and molybdenum, together with smaller additions of titanium and aluminum. This composition provides a strong combination of high mechanical strength, good corrosion resistance and favorable fabrication characteristics.

 

Chemical Composition (Inconel 718 / Alloy 718)

 

Ni %

Cr %

Nb+Ta %

Mo %

Mn %

Si %

Al %

Ti %

Co %

Cu %

Fe %

50.00 – 55.00

17.00 – 21.00

4.75 – 5.50

2.80 – 3.30

0.35 max.

0.35 max.

0.20 – 0.80

0.65 – 1.15

1.00 max.

0.30 max.

Balance

 

Mechanical Properties (Solution Annealed)

 

Product Form

Rp0.2, MPa

Rm, MPa

Elongation [%]

Hardness [HB]

Density [g/cm3]

Round Bar

483

931

45

≈240*

8.2

Plate (AMS 5596)

≤724

≤1034

≥30

≈253*

8.2

* HB values are approximate conversions.

 

Applications

 

Industry

Most Common Products

Aerospace

Turbine discs, engine/turbine casings, fastening components

Energy / Gas Turbines

Turbine rings, turbine casings, formed sheet components

Space & Rocket Systems

Rocket propulsion components, liquid-fuel rocket parts, spacecraft components

Oil & Gas

Hanger/packer systems, completion tools, pump shafts

Automotive

Turbocharger heat shields, turbocharger gaskets, high-temperature turbocharger components

Fasteners / Machinery

High-strength bolts and screws, springs, fastening components

Industrial Manufacturing / Tooling

Forging dies, extrusion tooling, hot-cutting/shearing tools

 

Additional Information

 

Inconel 718 / Alloy 718 stands out for its comparatively good weldability despite its high strength, and it shows lower susceptibility to strain-age cracking than many other precipitation-hardened nickel superalloys. The alloy can be hot- and cold-formed; however, its high strength and work-hardening tendency require suitable tooling and controlled cutting conditions during machining. Aging after solution annealing significantly increases its mechanical strength. Inconel 718 / Alloy 718 is widely used where high mechanical strength is required from cryogenic conditions up to about 650°C, and may also be considered for service approaching 700°C under specific design and operating conditions.

 

Specification

Inconel 718, Alloy 718, 2.4668, N07718.

 

Standards

Product Form

ASTM

AMS

Round Bar

ASTM B637

AMS 5662, AMS 5663, AMS 5664

Plate / Sheet / Strip

ASTM B670

AMS 5596, AMS 5597


Alternative Grades


Useful Links


Note: The information provided in this data sheet is for informational purposes only; no liability is accepted.

Inconel 718, Alloy 718, 2.4668, N07718Inconel 718, Alloy 718, 2.4668, N07718Inconel 718, Alloy 718, 2.4668, N07718