China HB K412 航空用高温合金热处理工艺 and Mechanical Properties, Chemical Element, Cross Reference.
Element | Min | Max | Similar |
---|---|---|---|
S | - | 0.0090 | - |
P | - | 0.0150 | - |
Si | - | 0.6000 | - |
Mn | - | 0.6000 | - |
V | - | 0.3000 | - |
B | 0.0050 | 0.0100 | - |
Fe | - | 8.0000 | - |
Ti | 1.6000 | 2.3000 | - |
Al | 1.6000 | 2.2000 | - |
Mo | 3.0000 | 4.5000 | - |
W | 4.5000 | 6.5000 | - |
Ni | - | - | - |
Cr | 14.0000 | 18.0000 | - |
C | 0.1100 | 0.1600 | - |
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) |
---|---|---|---|---|---|---|
891 (≥) | 197 (≥) | 22 | 43 | 12 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 324 |
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 |
---|---|---|---|---|---|---|---|
23 | - | - | 0.32 | - | |||
677 | 289 | - | 43.3 | 234 | - | ||
974 | - | 21 | 32.2 | 223 | 333 |
Heat treated : 1893°C - 1727°C
Grade | Standard | Country | Application |
---|---|---|---|
ASTM 5140 | |||
AISI 201 | |||
AISI 202 | |||
1.2767 | |||
17-4PH | |||
AISI 1052 | |||
AISI 416Se | |||
AISI 1330 | |||
AISI 205 Stainless Steel | |||
AISI A10 | |||
AISI A2 | |||
AISI A3 | |||
AISI A4 | |||
1.0036 | |||
1.0037 | |||
SAE J403 | |||
UNS G10100 | |||
AMS 4924 | |||
ASTM A36 | |||
Electrode 100S-1 |
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