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China HB K4130 航空用高温合金热处理工艺 and Mechanical Properties, Chemical Element, Cross Reference.

Datasheet for: Metals: K4130 / K4130
Category Grade Standard Region/Area Standard Content
Metals K4130 HB/Z 140 China 航空用高温合金热处理工艺

Chemical composition(mass fraction)(wt.%) of the K4130

Element Min Max Similar
C - 0.1000 -
Cr 20.0000 23.0000 -
Ni - - -
Co - 1.0000 -
W - 0.2000 -
Mo 9.0000 10.5000 -
Al 0.7000 0.9000 -
Ti 2.4000 2.8000 -
Fe - 0.5000 -
Nb - 0.2500 -
Mn - 0.6000 -
Si - 0.6000 -
Ag - 0.0005 -
Bi - 0.0001 -
Pb - 0.0010 -

Mechanical Properties of steel grade K4130

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)
289 (≥) 114 (≥) 22 23 12 Solution and Aging, Annealing, Ausaging, Q+T,etc 411

Physical Properties of steel grade K4130

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
41 - -     0.23 -  
635 742 - 42.3 442   -  
687 - 44 31.2   334 133

Heat Treatment of steel grade K4130

Heat treated : 1244°C - 1927°C

Technological Curves of steel grade K4130

Cross Reference Table (Equivalent Grade) of K4130

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