Inconel 718
Material Data Sheet
Inconel 718 is a vacuum melted (double or triple melted for cleanliness) precipitation-hardening nickel alloy.
It maintains its high strength, oxidation, and corrosion resistance while maintaining its superior ductility under extreme environments. Inconel 718 is used in many industries for critical applications including aerospace, defense and petrochemical. Inconel 718 is characterized by having superb tensile, fatigue, creep and rupture strength at temperatures up to 1290 °F (980 °C). This makes it ideal for many high-temperature applications such as gas turbine, instrumentation, and power/process industry parts. It also has excellent utility for cryogenic applications. Parts built from Inconel 718 can be easily post-hardened through precipitation-hardening heat treatments. In both traditional and age-hardened states, the parts can be machined, spark eroded, welded, micro shot-peened, polished and coated if required.
The 4 main Inconel 718 bar stocking positions taken by Alloys International, Inc. are in accordance with AMS 5662 solution treated, AMS 5663 and 5664 solution treated and aged and NACE MR-01-75. For other forms please see the chart below.
NACE MR-01-75, produced in accordance with the API (American Petroleum Institute), is in a separate category from the AMS material, with adjusted chemistry that allows for the material to have a different range of characteristics. It also employs an adjusted annealing and aging temperature, which produces a product with lower mechanicals, larger grain and increased toughness. This is generally preferred for many oil, offshore, and OEM applications.
Element | Content (%) |
---|---|
Iron, Fe | Balance |
Nickel, Ni | 50.0 – 55.0 |
Chromium, Cr | 17.0 – 21.0 |
Niobium, Nb | 4.7 – 5.5 |
Molybdenum, Mo | 2.8 – 3.3 |
Cobalt, Co | ≤ 1.0 |
Titanium, Ti | 0.65 – 1.15 |
Manganese, Mg | ≤ 0.35 |
Phosphorus, P | ≤ 0.35 |
Copper, Cu | ≤ 0.3 |
Aluminum, Al | 0.2 – 0.8 |
Carbon, C | ≤ 0.08 |
Sulfur, S | ≤ 0.015 |
Properties | Metric | Imperial |
---|---|---|
Density | 8.192 g/cm3 | 0.296 lb/in3 |
Melting Range | 1370-1430°C | 2500-2600°F |
Specific Gravity | 8.19 | 8.19 |
Properties | Metric | Imperial |
---|---|---|
Tensile Strength, Ultimate | 1375 MPa | 199000 psi |
Tensile Strength, Yield | 1100 MPa | 160000 psi |
Elongation at Break | 25% | 25% |
Cryogenic storage tanks
Downhole shafting
Gas turbine components
High strength bolting
Jet engines
Pump parts
Pump shafts
Rocket motors
Thrust reversers
Nuclear fuel element spacers
Key Words:IN718, inco 718, inco-718, inconel-718, INCONEL 718, AFNOR NC 19 Fe Nb, UNS N07718; ASTM B637, B670; ASME Boiler Code Sections I, III; AMS 5589, AMS 5590, AMS 5596, AMS 5597, AMS 5662, AMS 5663, AMS 5664, AMS 5832, Werkstoff Nr. 2.4668; WL Nr. 2.4668; MIL-N-24469; NACE MR-01-75; AECMA Pr EN 2404, 2405, 2407, 2408, 2952, 2961, 3219