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- ATI Allvac® Ti-17 Titanium Alloy, Heat Treatment: 899°C (1650°F) + Age
ATI Allvac® Ti-17 Titanium Alloy, Heat Treatment: 899°C (1650°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® Ti-17 Titanium Alloy, Heat Treatment: 899°C (1650°F) + Age.pdf  |
| Price | EMAIL US sales@lookpolymers.com |
Material Notes:
Data provided by Allvac.Applications: Compressor discs, heavy section forgings for gas turbine engine components. High tensile strength and good fracture toughness.
| 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 | 1138 MPa | 165100 psi | |
| Tensile Strength, Yield | 1069 MPa @Strain 0.200 % |
155000 psi @Strain 0.200 % |
|
| Elongation at Break | 12 % | 12 % | |
| Reduction of Area | 25 % | 25 % |
| Component Elements Properties | Metric | English | Comments |
|---|---|---|---|
| Aluminum, Al | 5.0 % | 5.0 % | |
| Carbon, C | 0.030 % | 0.030 % | |
| Chromium, Cr | 4.0 % | 4.0 % | |
| Copper, Cu | 0.050 % | 0.050 % | |
| Hydrogen, H | <= 0.015 % | <= 0.015 % | |
| Iron, Fe | 0.15 % | 0.15 % | |
| Manganese, Mn | 0.050 % | 0.050 % | |
| Molybdenum, Mo | 4.0 % | 4.0 % | |
| Nitrogen, N | 0.020 % | 0.020 % | |
| Oxygen, O | 0.11 % | 0.11 % | |
| Tin, Sn | 2.0 % | 2.0 % | |
| Titanium, Ti | 83 % | 83 % | as balance |
| Zirconium, Zr | 2.0 % | 2.0 % |
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