Inconel 718 Alloy Sheet, 1 mm, 2.4668, UNS N07718, 400 × 800 mm

Description

• Material: W. Nr. 2.4668; UNS N07718; Alloy 718
• Applications: aerospace; gas turbines; nuclear reactors; pumps; offshore technology; high-strength fasteners; heat-resistant tools
• Properties: excellent corrosion resistance; high strength; excellent weldability; good resistance to post-weld cracking
• Excellent creep strength at temperatures up to 700 C
• High fatigue strength; good mechanical properties at high and low temperatures
• Density: 8.2 g/cm; melting point: 1,260 C
• Width and length tolerance: 2 mm

Warning: sharp edges. Sheets are cut with a guillotine shear, and the edges are not deburred. Scratches on the surface cannot be ruled out. Product photos are for illustration only; the supplied cut pieces may differ. Inconel 718 is a precipitation-hardenable alloy consisting primarily of nickel, chromium, and iron, with niobium, molybdenum, aluminum, and titanium as additional components. The addition of niobium, titanium, and aluminum enables the alloy to be precipitation hardened. In the solution-annealed condition, 2.4668 can be formed and processed well. The material also offers excellent corrosion resistance at high and low temperatures and is not susceptible to pitting or stress-corrosion cracking. It has very good creep strength and high fatigue strength. It is also very weldable and provides good oxidation resistance up to 1,000 C. Inconel 718 is used primarily in aerospace applications, including for engines, gas turbines, and housings. The material is also used in offshore technology and marine engineering systems. Other applications for 2.4668 include the oil and gas industry, nuclear reactors, springs, and high-strength fasteners. Inconel 718 is characterized by good formability and precipitation hardenability, good processing properties in the solution-annealed condition, excellent corrosion resistance at high and low temperatures, resistance to pitting and stress-corrosion cracking, very good creep strength, high fatigue strength, very good weldability, and good oxidation resistance up to 1,000 C.

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