Inconel® 718 Sheet
Inconel®
Inconel 718 is a precipitation-harden able, nickel-chromium alloy containing also-significant amounts of iron, niobium and molybdenum, along with lesser amounts of aluminum and titanium. It combines corrosion resistance and high strength with outstanding weld ability, including resistance to post weld cracking. Inconel 718 has excellent creep-rupture strength at temperatures to 1300°F (700°C).
Inconel 718 is used in gas turbines, rocket motors, space-craft, nuclear reactors, pumps and tooling. Standard product forms are round, flats, extruded section, pipe, tube, forging stock, plate, sheet, strip and wire.
Unit of Measure
Items |
/Asset/sheet.jpg I718-078 Inconel® 718 Sheet |
/Asset/sheet.jpg I718-093 Inconel® 718 Sheet |
/Asset/sheet.jpg I718-104 Inconel® 718 Sheet |
/Asset/sheet.jpg I718-125 Inconel® 718 Sheet |
/Asset/sheet.jpg I718-134 Inconel® 718 Sheet |
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Material | N/A Inconel® | |||||||||
Shapeform | N/A Sheets | |||||||||
Thickness | N/A 0.078 inches1.9812 mm | N/A 0.093 inches2.3622 mm | N/A 0.104 inches2.6416 mm | N/A 0.125 inches3.1750 mm | N/A 0.134 inches3.4036 mm | |||||
Alloy | N/A Inconel® 718 | |||||||||
Basic Composition | N/A 18.0% Chrominum 18.5% Iron 3.0% Molybdenum 5.0% Niobium 54.0% Nickel | |||||||||
Density | N/A 0.296 lbs/in³8.19 g/cm³ | |||||||||
ASTM Specification | N/A ASTM B670 SAE 5596 SAE 5597 UNS N07718 | |||||||||
Melting Temperature Range | N/A 2300 to 2437 ºF1260 to 1336 ºC | |||||||||
Rupture Strength (1000 h at 1100°F/595°C) | N/A 110000 psi760 MPa | |||||||||
Rupture Strength (1000 h at 1200°F/650°C) | N/A 86000 psi590 MPa | |||||||||
Rupture Strength (1000 h at 1300°F/705°C) | N/A 53000 psi370 MPa | |||||||||
Rupture Strength (1000 h at 1400°F/760°C) | N/A 24000 psi170 MPa | |||||||||
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