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- ATI Allvac® 6-2-4-6 Titanium Alloy, Heat Treatment: 885°C (1625°F) + Age
ATI Allvac® 6-2-4-6 Titanium Alloy, Heat Treatment: 885°C (1625°F) + Age
| Category | Metal , Nonferrous Metal , Titanium Alloy , Alpha/Beta Titanium Alloy |
| 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® 6-2-4-6 Titanium Alloy, Heat Treatment: 885°C (1625°F) + Age.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Intermediate-temperature jet engine applications. Blades, discs, spacers, seals. Standard, rotor/premium grades.
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 4.65 g/cc | 0.168 lb/in³ |
| Mechanical Properties | Metric | English | Comments |
|---|---|---|---|
| Hardness, Brinell | 351 | 351 | Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball |
| Hardness, Knoop | 382 | 382 | Estimated from Rockwell C value. |
| Hardness, Rockwell C | 38 | 38 | |
| Hardness, Vickers | 367 | 367 | Estimated from Rockwell C value. |
| Tensile Strength, Ultimate | 1172 MPa | 170000 psi | |
| Tensile Strength, Yield | 1104 MPa @Strain 0.200 % |
160100 psi @Strain 0.200 % |
|
| Elongation at Break | 10 % | 10 % | |
| Reduction of Area | 15 % | 15 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Aluminum, Al | 6.0 % | 6.0 % | |
| Carbon, C | <= 0.10 % | <= 0.10 % | |
| Hydrogen, H | <= 0.015 % | <= 0.015 % | |
| Iron, Fe | 0.10 % | 0.10 % | |
| Molybdenum, Mo | 6.0 % | 6.0 % | |
| Nitrogen, N | 0.020 % | 0.020 % | |
| Oxygen, O | 0.12 % | 0.12 % | |
| Tin, Sn | 2.0 % | 2.0 % | |
| Titanium, Ti | 82 % | 82 % | as balance |
| Zirconium, Zr | 4.0 % | 4.0 % |
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