Stainless Steel Bars for Compressor and Turbine Airfoils
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
C | - | 0.07 | ||
Mn | - | 1.00 | ||
Si | - | 1.00 | ||
P | - | 0.04 | ||
S | - | 0.03 | ||
Cr | 15.50 | 17.50 | ||
Ni | 3.00 | 5.00 | ||
Mo | - | - | ||
Cu | 3.00 | 5.00 | ||
Nb | 0.15 | 0.45 |
Stainless Steel Bars for Compressor and Turbine Airfoils
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) |
---|---|---|---|---|---|---|
375 (≥) | 235 (≥) | 22 | 42 | 32 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 314 |
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 |
---|---|---|---|---|---|---|---|
912 (≥) | 986 (≥) | 41 | 44 | 32 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 412 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
681 | 228 | 612 |
We can customize the production of A 1028 S17400 grade, contact us for the best solution.
–sales@specificsteel.com