XC38 Air 9160/C chemical information,mechanical properties, physical properties, mechanical properties, heat treatment, and Micro structure, etc. It also contains the use of XC38 Air 9160/C

AFNOR XC38 Air 9160/C

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This page is mainly introduced the XC38 Air 9160/C chemical information,mechanical properties, physical properties, mechanical properties, heat treatment, and Micro structure, etc. It also contains the use of XC38 Air 9160/C,such as it is commonly used in bars, sheet,plates, steel coils, steel pipes,forged and other materials application.
XC38 Air 9160C wrought steels used in aeronautical constructions

Chemical composition(mass fraction)(wt.%)

Elements Min.(≥) Max.(≤) Similar Remarks
C 0.35  0.40
Si 0.10  0.40
Mn 0.50  0.80
P   0.035
S   0.035

Mechanical Properties

Tensile strength 922~204 σb/MPa
Yield Strength 419 σ 0.2 ≥/MPa
Elongation 00 δ5≥(%)
ψ - ψ≥(%)
Akv - Akv≥/J
HBS 340~469 -
HRC 30 -

Physical Properties

Thermal expansion 13-35 e-6/K
Thermal conductivity 69-21 W/m.K
Specific heat 450-460 J/kg.K
Melting temperature 9156-7356 째C
Density 4371-4170 kg/m3
Resistivity 0.50-0.60 Ohm.mm2/m
     

Heat Treatment Regime

Annealing

Quenching

Tempering

Normalizing

Q & T

Size Availability

Steel Grade Specification Processing range(mm)
XC38 Air 9160/C Aviation and Aero Steel Round Bar and Hollow Bar Φ1 to Φ2000
Square and Flat Steel Φ10 to Φ100
Plate and Sheet 0.08-800(Thickness)*10-1500(Width)*Length
Tube or Pipe OD:Φ4-410; WT:1-35 mm; Lenght:10-12000
Coil and Strip Steel THK:0.1mm Width:1500mm
Forged Ring/Cylindrical/Disk

Technical specification/standard for download

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