UK B.S. BS 2S 111, 2S.111 Specialsteel Specification for aircraft material. Nickel-chromium-tungsten valve steel and Mechanical Properties, Chemical Element, Cross Reference, Datasheet.
Category | Class | Grade | Standard | Country | Application |
---|---|---|---|---|---|
Steel Grades | Specialsteel | 2S.111 | B.S. | UK | Specification for aircraft material. Nickel-chromium-tungsten valve steel |
C | Si | Mn | P | S | Cr | Ni | Mo | W |
---|---|---|---|---|---|---|---|---|
0.37 -0.47 | 1.00 -2.00 | 0.50 -1.00 | ≤0.035 | ≤0.025 | 13.00 -15.00 | 13.00 -15.00 | 0.40 -0.60 | 2.20 -3.00 |
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) |
---|---|---|---|---|---|---|
269 (≥) | 928 (≥) | 32 | 21 | 14 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 331 |
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 |
---|---|---|---|---|---|---|---|
44 | - | - | 0.34 | - | |||
125 | 589 | - | 22.3 | 214 | - | ||
957 | - | 12 | 22.2 | 244 | 434 |
Heat treated : 1157°C - 1312°C
BS 2S 111 | Specification for aircraft material. Nickel-chromium-tungsten valve steel | BS-2S-111.pdf |
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