| Element | Content(%) |
|---|---|
| Ti | Remaining |
| V | 9%-11% |
| Al | 2.6%-3.4% |
| Fe | 1.6%-2.2% |
| O | ≤0.13% |
| C | ≤0.05% |
| N | ≤0.05% |
| H | ≤0.015% |
| Y | ≤0.005% |
| Left each | ≤0.1 |
| Left total | ≤0.3 |
Ti-10V-2Fe-3Al is known as Ti 10-2-3, is a non-ferrous near-beta titanium alloy featuring an excellent combination of strength, ductility, fracture toughness and high cycle fatigue strength.
IIt is typically used in the aerospace industry for critical aircraft structures, such as landing gear components and has become more popular for aerospace applications due to its improved heat treatability. Ti-10V-2Fe-3Al offers excellent combinations of strength, ductility, fracture toughness and high cycle fatigue strength.
| Element | Content(%) |
|---|---|
| Ti | Remaining |
| V | 9%-11% |
| Al | 2.6%-3.4% |
| Fe | 1.6%-2.2% |
| O | ≤0.13% |
| C | ≤0.05% |
| N | ≤0.05% |
| H | ≤0.015% |
| Y | ≤0.005% |
| Left each | ≤0.1 |
| Left total | ≤0.3 |
| Property | Value |
|---|---|
| Tensile strength | 1241 MPa min. |
| 0.2% offset yield strength | 1103 MPa min. |
| Elongation (4D) | 4% min. |
| Reduction of area | To be reported, except when using flat sheet specimens. |