Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)
Elements | Min.(≥) | Max.(≤) | Similar | Remarks |
---|---|---|---|---|
C | 0.04 | 0.08 | ||
Si | - | 0.50 | ||
Mn | - | 0.20 | ||
P | - | - | ||
S | - | 0.015 | ||
Cr | 15.50 | 17.50 | ||
Ni | 42.00 | 45.00 | ||
Mo | 2.80 | 3.80 | ||
Co | - | 2.00 | ||
Ti | 1.10 | 1.30 | ||
Fe | - | remaining | ||
Al | 1.10 | 1.30 | ||
Cu | - | 0.50 | ||
B | - | 0.005 | ||
Pb | - | 0.0015 | ||
Bi | - | 0.0001 | ||
Ag | - | 0.0005 | ||
Zr | 0.01 | 0.04 |
Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)
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) |
---|---|---|---|---|---|---|
781 (≥) | 197 (≥) | 11 | 34 | 12 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 133 |
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 |
---|---|---|---|---|---|---|---|
943 (≥) | 266 (≥) | 43 | 11 | 42 | Solution and Aging, Annealing, Ausaging, Q+T,etc | 424 | |
Temp. °C/°F |
Creep strain limit (10000h) (Rp1,0) N/mm2 |
Creep rupture strength (10000h) (Rp1,0) N/mm2 |
|||||
126 | 241 | 976 |
We can customize the production of HR55 grade, contact us for the best solution.
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