
VT22I Titanium (ВТ22И) is a high-strength, heat-treatable α+β titanium alloy used for heavily loaded parts where toughness, fatigue resistance, and long-term reliability are required. VT22I is supplied in wrought forms such as plate, bar, forgings, and stampings, and is typically selected for aerospace and heavy engineering applications that operate under high stress and demanding service conditions.
VT22I belongs to the VT22 family of high-alloyed titanium grades and is associated with high strength levels that depend on the supplied condition and heat treatment. In practice, the alloy is used when designers need a strong combination of strength, ductility, and section hardenability for large, load-bearing components.

VT22I is an α+β titanium alloy that uses β-stabilizing elements to achieve high strength after solution treatment and aging. When processed correctly, VT22I can be tuned to microstructures that balance strength with usable ductility for heavy-duty aerospace and industrial parts.
The best performance is typically achieved by controlled deformation and heat treatment that forms a stable (α + β) structure. Depending on the route (forging/rolling + solution treatment + aging), the alloy can be optimized toward higher strength or improved plasticity for large stampings and load-bearing parts.
| Grade : | VT22I |
| Classification : | Titanium wrought alloy |
| Application: | Large loaded stampings, increased plasticity |
| Foreign analogues: | No data |
VT22I is selected for heavy-load parts where high tensile strength and strong load-bearing capacity are required after proper heat treatment.
The alloy supports good fatigue performance under cyclic stress, making it suitable for aerospace structures and rotating assemblies.
Like many titanium alloys, VT22I provides good resistance to corrosion, helping extend service life in harsh environments.
VT22I is heat treatable and can be processed to achieve a targeted balance of strength and ductility depending on the application.
One practical advantage of VT22-family alloys is the ability to retain high strength through thicker sections when processed correctly.
Titanium’s low density supports weight reduction, which is critical for aerospace structures and high-performance engineering components.
GOST 1-90013 - 81
| Fe | C | Si | Cr | Mo | V | N | You | Al | Zr | O | H | Impurities |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 0.5 - 1.5 | up to 0.1 | up to 0.15 | 0.5 - 1.5 | 4 - 5.5 | 4 - 5.5 | up to 0.05 | 81.1 - 87.1 | 2.6 - 3.8 | up to 0.3 | up to 0.18 | up to 0.015 | other 0.3 |
Published property values can vary by product form and heat treatment. The table below keeps your structure while presenting the data in a clean, SEO-friendly way.
| Feature / Property | Typical Value / Observation | Source |
|---|---|---|
| Shape-Memory Effect (VT22I) | Recovered ~5% torsional strain after deformation and heating (quenched from β-field) | SpringerLink |
| Ultimate Tensile Strength (UTS, VT22 family) | ~1080 – 1280 MPa for plates (11–60 mm thickness) | Auremo |
| Elongation (VT22 family) | ≥ 6% | Auremo |
| Reduction of Area (VT22 family) | ≥ 16% | Auremo |
| Bars (Hot-Rolled, Quenched & Aged – VT22 family) | UTS ≥ 1280 MPa, Elongation ≥ 7% (for 10–12 mm section) | Auremo |
Approximate physical and performance-related indicators associated with VT22I and the broader VT22 family:
| Property / Observation | Typical Value / Description | Source |
|---|---|---|
| Density | ~4600 kg/m³ (as reported for VT22 family) | Auremo |
| Hardenability | High — maintains strength through large section thickness (up to ~200 mm) | YMAWS |
| Ultimate Tensile Strength (indicative range) | ~1000 – 1300 MPa (depending on condition, heat treatment, and section) | Derived from VT22 family data |
| Elongation (indicative range) | ~6 – 10% | Derived from VT22 family data |
| Strength Retention | Good — supports high strength in thicker sections with proper processing | YMAWS |
| Processing Sensitivity | Requires precise heat treatment to achieve the desired balance of strength and ductility | — |
Overall, VT22I Titanium Alloy is positioned for heavy-load applications where high strength, section hardenability, and controlled ductility are required for long-term service.
Used for heavily loaded aircraft structures, landing gear components, and aerospace parts that require high strength with reliable fatigue performance.
Applied in high-performance systems where durability and long service life are required under demanding environments.
Suitable for corrosion-resistant assemblies and fittings in aggressive or saltwater-exposed environments.
Used for large stampings and heavy-duty components where section strength and toughness matter.
Russian Metals supplies VT22I titanium with support for product selection, documentation, and project-specific preparation.
Supply support for VT22I titanium in common wrought forms based on availability and project needs.
Precision cutting and sizing support to help you match drawing requirements and manufacturing flow.
Guidance for selecting condition and form factor based on loading, thickness, and performance expectations.
Note: Ti is the basis; Ti percentage is approximate.
σin - Tensile strength [MPa]
σT - Yield stress [MPa]
δ5 - Specific elongation at fracture [%]
ψ - Reduction of area [%]
KCU - Impact strength [kJ/m²]
HB - Brinell hardness [MPa]
T - Test temperature [Grade]
E - Young modulus [MPa]
α - Coefficient of linear expansion (20° - T) [1/Grade]
λ - Thermal (heat) condition coefficient [Watt/(m·Grade)]
ρ - Density [kg/m³]
C - Specific heat (range 20° - T) [J/(kg·Grade)]
R - Electrical resistance [Ohm·m]
For more information or to place an order, contact Russian Metals today. We supply GOST VT22I Titanium for industrial, defense, and aerospace requirements with documentation and project support.