Specification for stainless steel cold rolled sheet for aviation
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
C | 0.08 | 0.13 | ||
Si | - | 0.40 | ||
Mn | 0.50 | 0.90 | ||
P | - | 0.030 | ||
S | - | 0.025 | ||
Cr | 11.00 | 12.50 | ||
Ni | 2.00 | 4.00 | ||
N | 0.020 | 0.040 | ||
V | 0.25 | 0.40 |
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) |
---|---|---|---|---|---|---|
866 (≥) | 263 (≥) | 12 | 22 | 32 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 222 |
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 |
---|---|---|---|---|---|---|---|
642 (≥) | 595 (≥) | 22 | 41 | 43 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 333 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
295 | 957 | 246 |
We can customize the production of 1Cr12Ni3Mo2VN grade, contact us for the best solution.
–sales@specificsteel.com