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ATI Allvac® Nickelvac® C-263 Nickel Superalloy, Heat Treatment: 927°C (1700°F) Anneal
| Category | Metal , Nonferrous Metal , Nickel Alloy , Superalloy |
| Manufacturer | ATI Allvac |
| Trade Name | Nickelvac® |
| Port | Shanghai port,China |
| Trade Terms | FOB, CFR, CIF |
| Payment Terms | L/C, T/T, Western Union |
| Download PDF | ATI Allvac® Nickelvac® C-263 Nickel Superalloy, Heat Treatment: 927°C (1700°F) Anneal.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Ring components in jet engines.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 8.35 g/cc | 0.302 lb/in³ |
| Mechanical Properties | Metric | English | Comments |
|---|---|---|---|
| Hardness, Brinell | 278 | 278 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 301 | 301 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 28 | 28 | |
| Hardness, Vickers | 292 | 292 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 931 MPa | 135000 psi | |
| Tensile Strength, Yield | 517 MPa @Strain 0.200 % |
75000 psi @Strain 0.200 % |
|
| Elongation at Break | 30 % | 30 % | |
| Reduction of Area | 35 % | 35 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Aluminum, Al | 0.45 % | 0.45 % | |
| Carbon, C | 0.060 % | 0.060 % | |
| Chromium, Cr | 20 % | 20 % | |
| Cobalt, Co | 20 % | 20 % | |
| Molybdenum, Mo | 5.85 % | 5.85 % | |
| Nickel, Ni | 51 % | 51 % | as balance |
| Titanium, Ti | 2.15 % | 2.15 % |
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