TB6
China SMC GJB 1538A (2008) TB6 Aircraft structure with titanium alloy rod specifications and Mechanical Properties, Chemical Element, Cross Reference, Datasheet.
SMC TB6 SMC TB6 Datasheet
| Category | Class | Grade | Standard | Country | Application |
|---|---|---|---|---|---|
| Steel Grades | Specialsteel | TB6 | SMC | China | Aircraft structure with titanium alloy rod specifications |
Datasheet for:Steel Grades:Specialsteel:TB6
Chemical composition(mass fraction)(wt.%) of the TB6
Mechanical properties / Mechanische Eigenschaften / Caracteristiques mecaniques of grade TB6
| Yield Rp0.2 (MPa) |
Tensile Rm (MPa) |
Impact KV/Ku (J) |
Elongation A (%) |
Reduction in cross section on fracture Z (%) |
As-Heat-Treated Condition | Brinell hardness (HBW) |
|---|---|---|---|---|---|---|
| 651 (≥) | 692 (≥) | 32 | 11 | 11 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 223 |
| Temperature (°C) |
Modulus of elasticity (GPa) |
Mean coefficient of thermal expansion 10-6/(°C) between 20(°C) and | Thermal conductivity (W/m·°C) |
Specific thermal capacity (J/kg·°C) |
Specific electrical resistivity (Ω mm²/m) |
Density (kg/dm³) |
Poisson’s coefficient, ν |
|---|---|---|---|---|---|---|---|
| 21 | - | - | 0.41 | - | |||
| 334 | 534 | - | 14.3 | 234 | - | ||
| 544 | - | 32 | 42.2 | 444 | 212 |
Heat treated : 1884°C - 1569°C
The material does not have direct Metallography properties.
Directory is being updated.
Directory is being updated.
The material does not have direct Metallography properties.
Directory is being updated.
Directory is being updated.
Cross Reference Table(Equivalent Grade)
| Grade | Standard | Country | Application |
|---|---|---|---|
| TB6 | SMC | China |
Aircraft structure with titanium alloy rod specifications
|
Relevant standard
| Standard No. | Description | Download |
|---|---|---|
| GJB 1538A (2008) | Aircraft structure with titanium alloy rod specifications |
Contact Suppliers with your enquiries for TB6 any of the shape and size.