UNS N07718, W.Nr. 2.4668

 

Inconel® 718 is a precipitation-hardenable nickel-chromium alloy also containing significant amounts of iron, niobium and molybdenum along with lesser amounts of aluminium and titanium. The alloy combines corrosion resistance and high strength with oustanding weldability including resistance to post-weld cracking. Inconel® 718 has excellent creep rupture strength at temperatures to 700°C. We stock both solution annealed AMS 5662 and age hardened AMS 5663. The alloy is used in gas turbines, rocket motors, spacecraft, nuclear reactors and pumps. Recommended filler metal for welding is Inconel® 718.

 

Applications

Aerospace alloys
Motorsport
Oil & Gas
Land based turbines
 

Applications

  • Aerospace
  • Nuclear
  • Energy

FAQ

What are the main components of Inconel® 718?
Inconel® 718 primarily consists of nickel, chromium, iron, niobium, and molybdenum, with smaller amounts of aluminium and titanium.
What is the maximum temperature for creep rupture strength?
The alloy has excellent creep rupture strength at temperatures up to 700°C.
What is the recommended filler metal for welding Inconel® 718?
The recommended filler metal for welding Inconel® 718 is Inconel® 718 itself.
EXPERT ADVICE: Ensure proper welding techniques are used to avoid post-weld cracking in Inconel® 718.

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INCONEL® 718 AMS 5662/AMS 5663/AMS 5596 - Round Bar


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