China SMC GJB 1538A (2008), TB6 Specialsteel Aircraft structure with titanium alloy rod specifications and Mechanical Properties, Chemical Element, Cross Reference, Datasheet.
| Category | Class | Grade | Standard | Country | Application | 
|---|---|---|---|---|---|
| Steel Grades | Specialsteel | TB6 | SMC | China | Aircraft structure with titanium alloy rod specifications | 
| Ti | Al | V | Fe | C | N | H | O | Y | Others total | Total Others | 
|---|---|---|---|---|---|---|---|---|---|---|
| ≤Remainder | 2.6000 -3.4000 | 9.0000 -11.0000 | 1.6000 -2.2000 | ≤0.0500 | ≤0.0500 | ≤0.0125 | ≤0.1300 | ≤0.0050 | ≤0.1000 | ≤0.3000 | 
| 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) | 
|---|---|---|---|---|---|---|
| 755 (≥) | 484 (≥) | 34 | 13 | 32 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 243 | 
| 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 | 
|---|---|---|---|---|---|---|---|
| 24 | - | - | 0.21 | - | |||
| 245 | 765 | - | 44.3 | 222 | - | ||
| 331 | - | 24 | 32.2 | 442 | 431 | 
Heat treated : 1721°C - 1555°C
| GJB 1538A (2008) | Aircraft structure with titanium alloy rod specifications | GJB-1538A---(2008).pdf | 
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