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Germany WL 2.4639 Aerospace series-High temperature nickel alloy with approx.0.2 C-20 Cr-Part 1:Welding filler metal and Mechanical Properties, Chemical Element, Cross Reference.

Datasheet for: Metals: 2.4639 / 2.4639
Category Grade Standard Region/Area Standard Content
Metals 2.4639 WL 2.4639-1 Germany Aerospace series-High temperature nickel alloy with approx.0.2 C-20 Cr-Part 1:Welding filler metal

Chemical composition(mass fraction)(wt.%) of the 2.4639

Element Min Max Similar
C - 0.2500 -
Mn - 1.2000 -
S - 0.0100 -
Si - 0.5000 -
Ni - - -
Cr 18.0000 21.0000 -
Cu - 0.2000 -
Fe - 0.5000 -

Mechanical Properties of steel grade 2.4639

Yield
Rp0.2 (MPa)
Tensile
Rm (MPa)
Impact
KV/Ku (J)
Elongation
A (%)
Reduction in cross section on fracture
Z (%)
As-Heat-Treated Condition Brinell hardness (HBW)
486 (≥) 745 (≥) 12 44 13 Solution and Aging, Annealing, Ausaging, Q+T,etc 222

Physical Properties of steel grade 2.4639

Temperature
(°C)
Modulus of elasticity
(GPa)
Mean coefficient of thermal expansion 10-6/(°C) between 20(°C) and Thermal conductivity
(W/m·°C)
Specific thermal capacity
(J/kg·°C)
Specific electrical resistivity
(Ω mm²/m)
Density
(kg/dm³)
Poisson’s coefficient, ν
34 - -     0.22 -  
388 891 - 32.3 332   -  
669 - 24 14.2   141 433

Heat Treatment of steel grade 2.4639

Heat treated : 1953°C - 1887°C

Technological Curves of steel grade 2.4639

Cross Reference Table (Equivalent Grade) of 2.4639

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