16NCD13 Air 9160/C Aviation and Aero Steel to AIR 9160 C

16NCD13 Air 9160/C - Specification & Application

  • AIR 9160 C - wrought steels used in aeronautical constructions

wrought steels used in aeronautical constructions

Chemical composition(wt.%) of 16NCD13 Air 9160/C grade: to AIR 9160 C

Elements Min.(≥) Max.(≤) Similar Remarks
C 0.12 0.17
Si 0.15 0.40
Mn 0.30 0.60
P - 0.025
S - 0.020
Cr 0.80 1.00
Ni 3.00 3.50
Mo 0.20 0.30

16NCD13 Air 9160/C - Detail

16NCD13 Air 9160C wrought steels used in aeronautical constructions

Mechanical properties of grade 16NCD13 Air 9160/C AIR 9160 C

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)
737 (≥) 739 (≥) 42 41 31 Solution and Aging, Annealing, Ausaging, Q+T,etc 414

Physical properties of grade 16NCD13 Air 9160/C AIR 9160 C

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
949 (≥) 614 (≥) 23 14 44 Solution and Aging, Annealing, Ausaging, Q+T,etc 244
Temp.
°C/°F
Creep strain limit
(10000h)
(Rp1,0) N/mm2
Creep rupture strength
(10000h)
(Rp1,0) N/mm2
227 153 852

Equivalent Grade

Equivalent Products

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