Holes with internal threads are made by threadmilling. This page displays only the textof a material data sheet.To see MatWeb's complete datasheet for this material (includingmaterial property data, metalcompositions, material suppliers,etc), please click the button below. Users requiring more precise data for scientific or engineering INCONEL® 718 (UNS N07718/W.Nr. 2.4668; MIL-N-24469; NACE MR-01-75; AECMA Pr EN 2404, 2405, 2407, 2408, 2952, 2961, 3219, Precipitation Hardened. 2.4668; MIL-N-24469; NACE MR-01-75; AECMA Pr EN 2404, 2405, 2407, 2408, 2952, 2961, 3219, Tensile Strength, Ultimate, Precipitation Hardened prior to test, Tensile Strength, Yield, Precipitation Hardened. Mechanical Properties Nominal room-temperature mechanical properties of INCONEL alloy 625 are shown in Table 5. Follow the links below to view complete property … Specialty Alloys comprise a broad group of materials that deliver properties for more demanding applications, use more exotic or expensive materials, or require special processes to manufacture. Developed in the early 1960's, IN718 is still considered the material of choice for the majority of aircraft engine components with service temperatures below 1200°F (650°C). 2.4668; WL Nr. The alloy resists a wide range of severely corrosive environments and is especially resistant to pitting and crevice corrosion. Introduction. Alloy 718 is an austenitic nickel-base superalloy which is used in applications requiring high strength to approximately 1400°F (760°C) and oxidation resistance to approximately 1800°F (982°C). It combines corrosion resistance and high strength with outstanding weldability including resistance to postweld cracking. Forms: round, flat, extruded section, pipe, tube, forging stock, plate, sheet, strip and wire. INCONEL® alloy 718 (UNS N07718/W.Nr. Common Trade Names: Inconel 718, Alloy 718, Nickel 718, Nicrofer 5219, Alvac 718, Haynes 718, Altemp 718. INCONEL 718 superalloy (IN718) is an age-hardenable Ni-Cr austenitic material with a wide service temperature range from −257 °C to 704 °C (Special Metals, 2007).Since IN718 was developed in the 1960s, the combination of high tensile, fatigue and creep-rupture strength, excellent oxidation resistance and outstanding resistance to postweld … Cold-forming properties and practices are essentially the same for INCOLOY alloy 825 as for INCONEL alloy 600. Inconel 718 is a nickel-based precipitation-hardening alloy designed for very high yield strength, tensile strength and creep rupture properties at temperatures up to 1300ºF (705ºC.) Data provided by the manufacturer, Special Metals. Alloy 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. error. For service above 1200°F, either annealed or solution-treated material will give best service. It combines corrosion resistance and high strength with outstanding weldability including resistance to postweld cracking. Applications: Aerospace, gas turbines, rocket motors, spacecraft, space shuttles, nuclear reactors, pumps, turbo pump seals, and tooling. INCONEL® alloy 718 4 Table 6 - Mechanical Properties Aged Material for Oil Tool Applications Room Temperature Tensile and Hardness, and Room Temperature and -75°F Impact Diameter, in. 2.4668; WL Nr. 2.4668) is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. The age-hardenable alloy can be readily fabricated, even into complex parts. INCONEL® alloy 600 3 Table 6 - Typical Mechanical-Property Rangesa Rod and Bar Cold-Drawn Annealed 80-100 550-690 25-50 170-345 55-35 65-85B As-Drawn 105-150 725-1035 80-125 550-860 30-10 90B-30C Please use one of the following formats to cite this article in your essay, paper or report: APA. INCONEL alloy 718 is one of the many nickel-based superalloys supplied by Corotherm. Nickel Alloy 718 – Properties, Composition, Heat … Inconel 718 is a precipitation-hardenable nickel-chromium alloy containing also significant amounts of iron, niobium, and molybdenum along with lesser amounts of aluminum and titanium. Applications: Aerospace, gas turbines, rocket motors, spacecraft, space shuttles, nuclear reactors, pumps, turbo pump seals, and tooling. It combines corrosion resistance and high strength with outstanding weldability including resistance to postweld cracking. Elongation at Break, Precipitation Hardened prior to test. 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