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- ATI Allvac® 706 Nickel Superalloy, Heat Treatment: 954°C (1750°F) + Age
ATI Allvac® 706 Nickel Superalloy, Heat Treatment: 954°C (1750°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® 706 Nickel Superalloy, Heat Treatment: 954°C (1750°F) + Age.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Land based turbine wheels and spacers. Jet engine components.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 8.08 g/cc | 0.292 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 | 1241 MPa | 180000 psi | |
| Tensile Strength, Yield | 1035 MPa @Strain 0.200 % |
150100 psi @Strain 0.200 % |
|
| Elongation at Break | 15 % | 15 % | |
| Reduction of Area | 25 % | 25 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Carbon, C | 0.030 % | 0.030 % | |
| Chromium, Cr | 16 % | 16 % | |
| Iron, Fe | 37 % | 37 % | as balance |
| Nickel, Ni | 42 % | 42 % | |
| Niobium, Nb (Columbium, Cb) | 2.9 % | 2.9 % | |
| Titanium, Ti | 1.8 % | 1.8 % |
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