Steel Forgings, Stainless, 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 |
Steel Forgings, Stainless, 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) |
---|---|---|---|---|---|---|
666 (≥) | 826 (≥) | 33 | 12 | 11 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 312 |
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 |
---|---|---|---|---|---|---|---|
258 (≥) | 675 (≥) | 43 | 33 | 22 | 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 |
|||||
233 | 163 | 561 |
We can customize the production of A 982 S17400 grade, contact us for the best solution.
–sales@specificsteel.com