wrought steels used in aeronautical constructions
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
C | - | 0.18 | ||
Si | - | 0.55 | ||
Mn | - | 1.50 | ||
P | - | 0.040 | ||
S | - | 0.040 | ||
Al | 0.02 | - |
E26-4 E 36-4 XES Air 9160C wrought steels used in aeronautical constructions
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) |
---|---|---|---|---|---|---|
813 (≥) | 556 (≥) | 44 | 33 | 33 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 242 |
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 |
---|---|---|---|---|---|---|---|
435 (≥) | 921 (≥) | 23 | 43 | 44 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 134 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
469 | 558 | 636 |
We can customize the production of E26-4 XES grade, contact us for the best solution.
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