Mainly used in the manufacture of aircraft engine working temperature in turbine blade and gas turbine blade below 750 DEG C; for fasteners
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
Ni | 63.00 | - | ||
C | - | 0.25 | ||
Mn | - | 1.50 | ||
Fe | - | 2.00 | ||
S | - | 0.01 | ||
Si | - | 0.50 | ||
Cu | 27.00 | 33.00 | ||
Al | 2.30 | 3.15 | ||
Ti | 0.35 | 0.85 |
Mainly used in the manufacture of aircraft engine working temperature in turbine blade and gas turbine blade below 750 DEG C; for fasteners, manufacturing ship spring; chemical equipment of the pump, valve parts; papermaking equipment on the scraping blade.
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) |
---|---|---|---|---|---|---|
817 (≥) | 751 (≥) | 31 | 34 | 34 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 443 |
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 |
---|---|---|---|---|---|---|---|
592 (≥) | 216 (≥) | 32 | 23 | 33 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 432 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
761 | 215 | 438 |
We can customize the production of MONEL K-500 grade, contact us for the best solution.
–sales@specificsteel.com