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- ATI Allvac® 718 Nickel Superalloy, Heat Treatment: 982°C (1800°F) + Age
ATI Allvac® 718 Nickel Superalloy, Heat Treatment: 982°C (1800°F) + Age
| Category | Metal , Nonferrous Metal , Nickel Alloy , Superalloy |
| Manufacturer | ATI Allvac |
| Trade Name | |
| Port | Ningbo port,China |
| Trade Terms | FOB, CFR, CIF |
| Payment Terms | L/C, T/T, Western Union |
| Download PDF | ATI Allvac® 718 Nickel Superalloy, Heat Treatment: 982°C (1800°F) + Age.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Jet engine rings, discs, shafts, compressor blades, seals, spacers. Fasteners, nuclear, oil & gas components.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 8.19 g/cc | 0.296 lb/in³ |
| Mechanical Properties | Metric | English | Comments |
|---|---|---|---|
| Hardness, Brinell | 389 | 389 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 425 | 425 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 42 | 42 | |
| Hardness, Vickers | 407 | 407 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 1345 MPa | 195100 psi | |
| Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
|
| Elongation at Break | 22 % | 22 % | |
| Reduction of Area | 35 % | 35 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Aluminum, Al | 0.50 % | 0.50 % | |
| Carbon, C | 0.020 % | 0.020 % | |
| Chromium, Cr | 19 % | 19 % | |
| Iron, Fe | 17 % | 17 % | as balance |
| Molybdenum, Mo | 3.1 % | 3.1 % | |
| Nickel, Ni | 54 % | 54 % | |
| Niobium, Nb (Columbium, Cb) | 5.2 % | 5.2 % | |
| Titanium, Ti | 0.90 % | 0.90 % |
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