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.
Documents
Applications
Applications
- Aerospace
- Nuclear
- Energy
FAQ
What is Inconel® 718 used for?
What are the temperature capabilities of Inconel® 718?
What filler metal is recommended for welding Inconel® 718?
INCONEL® 718 AMS 5662/AMS 5663/AMS 5596 - Sheet/Plate
- Brand: GTeek
- Product Code: INCONEL® 718 AMS 5662/AMS 5663/AMS 5596 - Sheet/Plate
- Availability: In Stock
Related Products
INCONEL® 718 AMS 5662/AMS 5663/AMS 5596 - Sheet/Plate
UNS N06600, W.Nr. 2.4816 INCONEL® (nickel-chromium-iron) alloy 600 is a standard engineering material for applications which require resistance to corrosion and heat. The alloy also has excellent mechanical properties and presents the desirable combination of high strength and good workability. The high nickel content gives the alloy resistance to corrosion by many organic and inorganic compounds and also makes it virtually immune to chloride-ion stress-corrosion cracking..
INCONEL® 718 - Sheet/Plate
AWS A5.14 ERNiFeCr-2, UNS N07718, W.Nr. 2.4667 Filler metal for welding INCONEL® 718 and X-750. ..
INCONEL® 718 - Sheet/Plate
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, n..
INCONEL® 718 AMS 5662/AMS 5663/AMS 5596 - Round Bar
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 AM..
INCONEL® 718 AMS 5662/AMS 5663/AMS 5596 - Tube
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 AM..
Tags: INCONEL®, 718, AMS, 5662/AMS, 5663/AMS, 5596, -, Sheet/Plate