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- ATI Allvac® 520 Nickel Superalloy, Heat Treatment: 1121°C (2050°F) + Age
ATI Allvac® 520 Nickel Superalloy, Heat Treatment: 1121°C (2050°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® 520 Nickel Superalloy, Heat Treatment: 1121°C (2050°F) + Age.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Land based gas turbine blades.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 8.22 g/cc | 0.297 lb/in³ |
| Mechanical Properties | Metric | English | Comments |
|---|---|---|---|
| Hardness, Brinell | 369 | 369 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 403 | 403 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 40 | 40 | |
| Hardness, Vickers | 386 | 386 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 1310 MPa | 190000 psi | |
| Tensile Strength, Yield | 828 MPa @Strain 0.200 % |
120000 psi @Strain 0.200 % |
|
| Elongation at Break | 20 % | 20 % | |
| Reduction of Area | 18 % | 18 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Aluminum, Al | 2.0 % | 2.0 % | |
| Boron, B | 0.0070 % | 0.0070 % | |
| Carbon, C | 0.050 % | 0.050 % | |
| Chromium, Cr | 19 % | 19 % | |
| Cobalt, Co | 12 % | 12 % | |
| Molybdenum, Mo | 6.0 % | 6.0 % | |
| Nickel, Ni | 57 % | 57 % | as balance |
| Titanium, Ti | 3.0 % | 3.0 % | |
| Tungsten, W | 1.0 % | 1.0 % |
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