Specifications
- Plate, Sheet & Strip: AMS 5596, AMS 5597
- Rod & Bar: ASTM B637, ASME SB637
- Seamless Pipe & Tube: ASTM B983
- Forgings: ASTM B637, ASME SB637
- Others: NACE MR0175, ISO 15156
Inconel® 718 was first used to make aerospace components in the 1960s. However, because it was readily available, the oil and gas industry used it in offshore wells for deeper drilling in higher temperatures and pressures exceeding 200 ksi (200,000 psi). Inconel 718’s relatively high melting point makes it well-suited to high-temperature applications of up to 700º C (1300º F).
While most metals become brittle, soft or oxidized when exposed to elevated temperatures, Inconel 718 forms a protective chromium oxide layer to prevent oxidation. A precipitation hardening process is required to produce the high tensile strengths. Typical applications include gas turbine parts and cryogenic storage tanks.
If your question isn’t answered below, download the complete technical data sheet here.
Physical Property | Imperial Units | Metric Units | ||
Density | RT | 0.297 lb/in3 | RT | 8.23 g/cm3 |
Melting Range | 2300-2435°F | — | 1260-1335°C | — |
Electrical Resistivity | RT | 47.5 μ0hm.in | RT | 121 μ0hm.cm |
200°F | 48.0 μ0hm.in | 100°C | 122 μ0hm.cm | |
400°F | 49.4 μ0hm.in | 200°C | 125 μ0hm.cm | |
600°F | 50.3 μ0hm.in | 300°C | 127 μ0hm.cm | |
800°F | 50.7 μ0hm.in | 400°C | 129 μ0hm.cm | |
1000°F | 51.6 μ0hm.in | 500°C | 130 μ0hm.cm | |
1200°F | 52.0 μ0hm.in | 600°C | 132 μ0hm.cm | |
1400°F | 52.2 μ0hm.in | 700°C | 132 μ0hm.cm | |
1600°F | 52.1 μ0hm.in | 800°C | 132 μ0hm.cm | |
1800°F | 52.4 μ0hm.in | 900°C | 133 μ0hm.cm | |
— | — | 1000°C | 133 μ0hm.cm | |
Thermal Conductivity | RT | 79 btu.in/h.ft2.°F | RT | 11.4 W/m.°C |
200°F | 87 btu.in/h.ft2.°F | 100°C | 12.6 W/m.°C | |
400°F | 100 btu.in/h.ft2.°F | 200°C | 14.3 W/m.°C | |
600°F | 112 btu.in/h.ft2.°F | 300°C | 15.9 W/m.°C | |
800°F | 124 btu.in/h.ft2.°F | 400°C | 17.5 W/m.°C | |
1000°F | 136 btu.in/h.ft2.°F | 500°C | 19.0 W/m.°C | |
1200°F | 148 btu.in/h.ft2.°F | 600°C | 20.6 W/m.°C | |
1400°F | 161 btu.in/h.ft2.°F | 700°C | 22.2 W/m.°C | |
1600°F | 173 btu.in/h.ft2.°F | 800°C | 23.8 W/m.°C | |
1800°F | 186 btu.in/h.ft2.°F | 900°C | 25.4 W/m.°C | |
— | — | 100°C | 27.1 W/m.°C | |
Mean Coefficient of Thermal Expansion |
70-200°F | 7.1 μin/in. °F | 25-100°C | 12.8 μm/m.°C |
70-400°F | 7.5 μin/in. °F | 25-200°C | 13.5 μm/m.°C | |
70-600°F | 7.7 μin/in. °F | 25-300°C | 13.8 μm/m.°C | |
70-800°F | 7.9 μin/in. °F | 25-400°C | 14.1 μm/m.°C | |
70-1000°F | 8.0 μin/in. °F | 25-500°C | 14.3 μm/m.°C | |
70-1200°F | 8.4 μin/in. °F | 25-600°C | 14.8 μm/m.°C | |
70-1400°F | 8.9 μin/in. °F | 25-700°C | 15.5 μm/m.°C | |
70-1600°F | 9.4 μin/in. °F | 25-800°C | 16.3 μm/m.°C | |
— | — | 25-900°C | 17.2 μm/m.°C | |
Dynamic Modulus of Elasticity | RT | 29.0 x 106 psi | RT | 200 GPa |
200°F | 28.4 x 106 psi | 200°C | 195 GPa | |
400°F | 27.6 x 106 psi | 300°C | 191 GPa | |
600°F | 26.7 x 106 psi | 400°C | 185 GPa | |
800°F | 25.8 x 106 psi | 500°C | 179 GPa | |
1000°F | 24.8 x 106 psi | 600°C | 173 GPa | |
1200°F | 23.7 x 106 psi | 700°C | 167 GPa | |
1400°F | 22.3 x 106 psi | 800°C | 159 GPa | |
1600°F | 20.2 x 106 psi | 900°C | 149 GPa | |
1800°F | 17.4 x 106 psi | 1000°C | 134 GPa |
RT= Room Temperature
Test Temperature |
Ultimate Tensile Strength |
0.2% Yield Strength | Elongation |
|||
°F | °C | ksi | MPa | ksi | MPa | % |
RT | RT | 200.5 | 1382 | 167.8 | 1157 | 20.6 |
800 | 427 | 173.1 | 1193 | 149.0 | 1027 | 22.6 |
1000 | 538 | 170.2 | 1173 | 145.9 | 1006 | 21.8 |
1200 | 649 | 162.5 | 1120 | 139.9 | 965 | 25.1 |
1400 | 760 | 117.3 | 809 | 104.9 | 723 | 12.1 |
1600 | 871 | 42.2 | 291 | 34.3 | 236 | 68.0 |
1800 | 982 | 14.1 | 97 | 9.6 | 66 | 129.9 |
Mill Annealed + 1325°F/8h/Furnace Cool to 1150°F/8h/Air Cool Total time: 18 hours
RT= Room Temperature
Test Temperature |
Ultimate Tensile Strength |
0.2% Yield Strength | Elongation |
|||
°F | °C | ksi | MPa | ksi | MPa | % |
RT | RT | 203.6 | 1404 | 174.7 | 1205 | 18.4 |
800 | 427 | 176.2 | 1215 | 155.4 | 1071 | 21.3 |
1000 | 538 | 172.3 | 1188 | 150.2 | 1036 | 20.7 |
1200 | 649 | 164.1 | 1131 | 144.3 | 995 | 16.3 |
1400 | 760 | 114.8 | 792 | 103.8 | 716 | 6.9 |
1600 | 871 | 39.9 | 275 | 34.0 | 234 | 81.8 |
1800 | 982 | 13.7 | 94 | 9.7 | 67 | 175.6 |
Mill Annealed + 1325°F/8h/Furnace Cool to 1150°F/8h/Air Cool
Total time: 18 hours
Form |
Ultimate Tensile Strength |
Yield Strength | Elongation |
||
ksi | MPa | ksi | MPa | % | |
Plate | 126.3 | 871 | 60.7 | 419 | 46.7 |
Sheet | 124.3 | 857 | 57.3 | 395 | 49 |
Temperature | Creep | Approximate Initial Stress to Produce Specified Creep in | ||||||
10h | 100h | 1,000h | ||||||
°F | °C | % | ksi | MPa | ksi | MPa | ksi | MPa |
1000 | 538 | 0.5 | 157 | 1083 | 146 | 1007 | 132 | 910 |
1 | 160 | 1103 | 150 | 1034 | 138 | 952 | ||
R | — | — | 165 | 1138 | 144 | 993 | ||
1100 | 593 | 0.5 | 140 | 965 | 126 | 869 | 108 | 745 |
1 | 143 | 986 | 130 | 896 | 112 | 772 | ||
R | 150 | 1034 | 134 | 924 | 115 | 793 | ||
1200 | 649 | 0.5 | 121 | 834 | 101 | 696 | 75 | 517 |
1 | 124 | 855 | 103 | 710 | 78 | 538 | ||
R | 130 | 896 | 105 | 724 | 87 | 600 | ||
1300 | 704 | 0.5 | 95 | 655 | 64 | 441 | 35 | 241 |
1 | 98 | 676 | 67 | 462 | 41 | 283 | ||
R | 106 | 731 | 76 | 524 | 46 | 317 | ||
1400 | 760 | 0.5 | 54 | 372 | 24 | 165 | 3.8 | 26 |
1 | 60 | 414 | 28 | 193 | 5.1 | 35 | ||
R | 70 | 483 | 37 | 255 | 17 | 117 |
*Samples were age hardened by treating at 1325°F (718°C)/8h/FC to 1150°F (621°C)/8h/AC
% Cold-Work | Average Hardness HRBW/ C |
0 | 92.4 HRBW |
10 | 27.2 HRC |
20 | 33.6 HRC |
30 | 36.9 HRC |
40 | 38.3 HRC |
50 | 39.2 HRC |
HRBW = Hardness Rockwell “B”, Tungsten Indentor.
HRC= Hardness Rockwell “C”.
Form | Hardness, HRBW | Typical ASTM Grain Size |
Sheet | 94 | 6 – 8 |
Plate | 93 | 5 – 8 |
All samples tested in solution-annealed condition.
HRBW = Hardness Rockwell “B”, Tungsten Indentor.
Inconel 718 is a high-strength, corrosion-resistant nickel-chromium alloy with traces of niobium, titanium and aluminum. Its increased toughness and strength are sustainable in cryogenic and elevated temperatures. The unique Inconel 718 composition allows for corrosion resistance in various environments, including seawater, hydrogen sulfide, CO2, elemental sulfur and chloride ions at vast temperatures.
It can be fabricated in the annealed or age-hardened condition. The annealed condition gives a slightly longer tool life, while the age-hardened condition gives a better finish and better chip action on chip breaker tools. Alloy 718 also features excellent welding properties compared to other Inconel alloys.
Inconel 718 provides several advantages, making it a preferred choice in various applications:
Inconel fasteners play a critical role in various industries, including:
Inconel fasteners come in various forms to suit different applications:
Inconel fasteners are highly valued for their resistance to oxidation and corrosion, strength at high temperatures, and thermal stability, making them suitable for various applications. They are also less likely to experience galvanic corrosion than other alloys. Choosing the right Inconel grade depends on these factors:
Most importantly, select the right supplier with a strong reputation and quality control. Ensure they provide essential documentation, like material test reports and compliance certificates, for traceability and assurance. Consult with the experts at Nickel Systems to help you find the right nickel alloy for your needs.