wrought steels used in aeronautical constructions
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
C | - | 0.03 | ||
Si | - | 1.00 | ||
Mn | - | 2.00 | ||
P | - | 0.035 | ||
S | - | 0.025 | ||
Cr | 17.00 | 19.00 | ||
Ni | 9.00 | 11.00 |
Z2CN18-10 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) |
---|---|---|---|---|---|---|
122 (≥) | 654 (≥) | 11 | 43 | 44 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 444 |
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 |
---|---|---|---|---|---|---|---|
467 (≥) | 962 (≥) | 14 | 23 | 42 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 211 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
689 | 739 | 721 |
We can customize the production of Z2CN18-10 Air 9160/C grade, contact us for the best solution.
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