VT5L
for the manufacture of castings, manufacturing parts control, set the fuselage internal welded parts and assemblies continuously operating (10,000 hours) at temperatures up to 400 ° C.
Classification
| Country | Section | Category |
|---|---|---|
| CIS, Russia, Ukraine | Titanium, titanium alloys | Foundry titanium alloys |
Chemical composition
| Standard | Fe, % | Si, % | Ti, % | Zr, % | Al, % | C, % | O, % | N, % | W, % | H, % |
|---|---|---|---|---|---|---|---|---|---|---|
| OST 1-90060-92 | < 0.35 | < 0.2 | 91.485–95.9 | < 0.8 | 4.1–6.2 | < 0.2 | < 0.2 | < 0.05 | < 0.2 | < 0.015 |
Information on suppliers
Physical characteristics
| Temperature, °C | $$E\cdot 10^{9}$$, $$MPa$$ |
|---|---|
| 20 | 118 |
Mechanical properties at 20 °C
Standards
| Standard | Description |
|---|---|
| OST 1-90060-92 |
Description of chemical elements
| Element | Units of measurement | Description |
|---|---|---|
| Fe | % | Iron |
| Si | % | Silicon |
| Ti | % | Titan |
| Zr | % | Zirconium |
| Al | % | Aluminium |
| C | % | Carbon |
| O | % | Oxygen |
| N | % | Nitrogen |
| W | % | Tungsten |
| H | % | Hydrogen |
Description of physical characteristics
| Parameter | Units of measurement | Description |
|---|---|---|
| $$E\cdot 10^{9}$$ | $$MPa$$ | Elastic modulus |
Description of mechanical properties
| Parameter | Units of measurement | Description |
|---|---|---|
| $$\sigma _{U}$$ | $$MPa$$ | Ultimate tensile strength |
| $$\epsilon_L$$ | % | Elongation at break (longitudinal) |
| $$KCU\cdot 10^{3}$$ | $$\frac{J}{m^2}$$ | Impact toughness |