VT6
Weldability without restrictions. The hardness of the rod VT6 after quenching and aging HB 10 -1 = 293 — 361 MPa. Hardness of VT6 punching after annealing HB 10 -1 = 255 — 341 MPa,
for the manufacture of large welded structures and precast aircraft, for the manufacture of cylinders operating under internal pressure in a wide range of temperatures from 196 to 450 ° C, and a number of other structural elements; class structure of α + β
Classification
| Country |
Section |
Category |
| CIS, Russia, Ukraine |
Titanium, titanium alloys |
Wrought Titanium Alloys |
Chemical composition
| Standard |
Fe, % |
Si, % |
Ti, % |
V, % |
Zr, % |
Al, % |
C, % |
O, % |
N, % |
H, % |
| GOST 19807-91 |
< 0.6 |
< 0.1 |
86.45–90.9 |
3.5–5.3 |
< 0.3 |
5.3–6.8 |
< 0.1 |
< 0.2 |
< 0.05 |
< 0.015 |
Information on suppliers
Physical characteristics
| Temperature, °C |
$$E\cdot 10^{9}$$, $$MPa$$ |
$$\alpha\cdot 10^{6}$$, $$K^{-1}$$ |
$$\varkappa$$, $$\frac{W}{m\cdot K}$$ |
$$\rho$$, $$\frac{kg}{m^3}$$ |
$$c\cdot 10^{-3}$$, $$\frac{J}{kg\cdot K}$$ |
$$R\cdot 10^{-6}$$, $$\Omega\cdot m$$ |
| 20 |
115 |
|
8.37 |
4450 |
|
1.6 |
| 100 |
|
8.4 |
9.21 |
|
|
1.82 |
| 200 |
|
8.7 |
10.88 |
|
0.586 |
2.02 |
| 300 |
|
9 |
11.7 |
|
0.67 |
2.12 |
| 400 |
|
10 |
12.56 |
|
0.712 |
2.14 |
| 500 |
|
|
13.82 |
|
0.795 |
|
| 600 |
|
|
15.49 |
|
0.879 |
|
Mechanical properties at 20 °C
| Rolling |
Standard |
Size, mm |
Tension |
Classifiers |
$$\sigma _{U}$$, $$MPa$$ |
$$\epsilon_L$$, % |
$$\psi$$, % |
$$KCU\cdot 10^{3}$$, $$\frac{J}{m^2}$$ |
Treatment |
| Sheet |
GOST 22178-76 |
|
|
annealing |
885 |
8 |
|
|
|
| Round |
GOST 26492-85 |
|
|
enhanced quality |
835–1050 |
6–10 |
20–30 |
300–400 |
|
| Round |
GOST 26492-85 |
|
|
|
1080 |
4 |
12 |
200 |
|
| Round |
GOST 26492-85 |
|
|
|
835–885 |
6–8 |
15–20 |
250 |
|
| Round |
GOST 26492-85 |
|
|
enhanced quality |
1080 |
6 |
20 |
250–300 |
|
| Stamping |
|
|
|
|
950–1100 |
10–13 |
35–60 |
400–800 |
|
| Plate |
GOST 23755-79 |
11–100 |
|
annealing |
835–1080 |
6 |
12–16 |
300 |
|
Brinell hardness number
| Rolling |
Standard |
Classifiers |
Value, HBW |
| Round |
|
Hardening, aging |
293–361 |
| Metal rolling |
|
annealing |
255–341 |
Technological Properties
Analogues
| Germany |
USA |
Japan |
France |
United Kingdom |
| 3.7164 |
6Al-4V |
SAT-64 |
T-A6V |
Ti-Al-V |
| 3.7165 |
Grade5 |
|
|
|
Standards
Description of chemical elements
| Element |
Units of measurement |
Description |
| Fe |
% |
Iron |
| Si |
% |
Silicon |
| Ti |
% |
Titan |
| V |
% |
Vanadium |
| Zr |
% |
Zirconium |
| Al |
% |
Aluminium |
| C |
% |
Carbon |
| O |
% |
Oxygen |
| N |
% |
Nitrogen |
| H |
% |
Hydrogen |
Description of physical characteristics
| Parameter |
Units of measurement |
Description |
| $$E\cdot 10^{9}$$ |
$$MPa$$ |
Elastic modulus |
| $$\alpha\cdot 10^{6}$$ |
$$K^{-1}$$ |
Coefficient of thermal (linear) expansion (range 20°C–T) |
| $$\varkappa$$ |
$$\frac{W}{m\cdot K}$$ |
Coefficient of thermal conductivity (the heat capacity of the material) |
| $$\rho$$ |
$$\frac{kg}{m^3}$$ |
The density of the material |
| $$c\cdot 10^{-3}$$ |
$$\frac{J}{kg\cdot K}$$ |
The specific heat of the material (range 20°C–T) |
| $$R\cdot 10^{-6}$$ |
$$\Omega\cdot m$$ |
Electrical resistivity |
Description of mechanical properties
| Parameter |
Units of measurement |
Description |
| $$\sigma _{U}$$ |
$$MPa$$ |
Ultimate tensile strength |
| $$\epsilon_L$$ |
% |
Elongation at break (longitudinal) |
| $$\psi$$ |
% |
Reduction in cross section on fracture |
| $$KCU\cdot 10^{3}$$ |
$$\frac{J}{m^2}$$ |
Impact toughness |
Designation of types of weldability
| Parameter |
Units of measurement |
Description |
| no limits |
|
Welding is performed without heating and without subsequent heat treatment |
| Boundedly welded |
|
Welding is possible with heating up to 100–120 °C and subsequent heat treatment |
| Difficult to weld |
|
For obtaining quality welded joints, additional operations are required: heating up to 200–300 °C for welding, heat treatment after welding — annealing |
| Not applicable for welded structures |
|
|