Allvac® 6-2-4-2 Titanium Alloy, Heat Treatment: 982°C (1800°F) + Age
Subcategory: Titanium Alloy; Nonferrous Metal; Alpha/Near Alpha Titanium Alloy
Key Words: UNS R54620; AMS 4919, 4975, 4976. MIL-T-9046, -9047, -81556, Ti-6Al-2Sn-4Zr-2Mo, Ti-6242; Ti-6-2-4-2; Allvac, an Allegheny Teledyne Company
Material Notes: Titanium content calculated as remainder. Data provided by Allvac. Applications: High-temp jet engines. Blades, discs, spacers, seals. High performance automotive valves. Standard, rotor/premium grades.
Available Properties |
- Density
- Hardness, Brinell
- Hardness, Knoop
- Hardness, Rockwell C
- Hardness, Vickers
- Tensile Strength, Ultimate
- Tensile Strength, Yield
- Elongation at Break
- Reduction of Area
|
|
|
|
Property Data |
This page displays only the text
of a material data sheet.
To see MatWeb's complete data
sheet for this material (including
material property data, metal
compositions, material suppliers,
etc), please click the button below. |
|
|
|
|