Z100CD-17 Air 9160/C Aviation and Aero Steel to AIR 9160 C

Z100CD-17 Air 9160/C - Specification & Application

  • AIR 9160 C - wrought steels used in aeronautical constructions

wrought steels used in aeronautical constructions

Chemical composition(wt.%) of Z100CD-17 Air 9160/C grade: to AIR 9160 C

Elements Min.(≥) Max.(≤) Similar Remarks
C 0.95 1.10
Si - 1.00
Mn - 1.00
P - 0.030
S - 0.020
Cr 16.00 18.00
Ni - 0.75
Mo 0.35 0.75

Z100CD-17 Air 9160/C - Detail

Z100CD-17 Air 9160C wrought steels used in aeronautical constructions

Mechanical properties of grade Z100CD-17 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)
433 (≥) 968 (≥) 31 22 34 Solution and Aging, Annealing, Ausaging, Q+T,etc 221

Physical properties of grade Z100CD-17 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
282 (≥) 263 (≥) 11 13 34 Solution and Aging, Annealing, Ausaging, Q+T,etc 411
Temp.
°C/°F
Creep strain limit
(10000h)
(Rp1,0) N/mm2
Creep rupture strength
(10000h)
(Rp1,0) N/mm2
484 774 251

Equivalent Products

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