Heat resistant materials for the extrusion processing of aluminum and aluminum alloys
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
C | 0.35 | 0.45 | ||
Si | 0.20 | 0.40 | ||
Mn | 1.30 | 1.60 | ||
P | - | 0.035 | ||
S | - | 0.035 | ||
Cr | 1.80 | 2.10 | ||
Mo | 0.15 | 0.25 | ||
V | - | - |
Heat resistant materials for the extrusion processing of aluminum and aluminum alloys
Proof strength Rp0.2 (MPa) |
Tensile strength Rm (MPa) |
Impact energy KV (J) |
Elongation at fracture A (%) |
Reduction in cross section on fracture Z (%) |
As-Heat-Treated Condition | Brinell hardness (HBW) |
---|---|---|---|---|---|---|
588 (≥) | 817 (≥) | 13 | 33 | 44 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 131 |
Property | Density kg/dm3 |
Temperature T °C/F |
Specific heat J / kgK |
Thermal conductivity W/mK |
Electric resistance µΩ·cm |
Modulus of elasticity kN/mm2 |
Expansion rate |
---|---|---|---|---|---|---|---|
241 (≥) | 995 (≥) | 21 | 41 | 41 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 433 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
753 | 883 | 721 |
We can customize the production of 1.2311 grade, contact us for the best solution.
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