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. The alloy is used in gas turbines, rocket motors, spacecraft, nuclear reactors and pumps. Recommended filler metal for welding is Inconel® 718.

 

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 aluminum and titanium.
What is the maximum temperature Inconel® 718 can withstand?
Inconel® 718 has excellent creep rupture strength at temperatures up to 700°C.
What applications is Inconel® 718 used for?
Inconel® 718 is used in gas turbines, rocket motors, spacecraft, nuclear reactors, and pumps.
EXPERT ADVICE: For optimal performance, ensure proper welding techniques are employed when using Inconel® 718, as it has outstanding weldability but can be sensitive to post-weld cracking.

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INCONEL® 718 - Wire


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