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2014 / 2014A

BS L168 / AlCu4SiMg / 2014 / 2014A / T6

Chemical Properties % Value
Silicon (Si)0,50 - 0,90
Chromium (Cr)0,00 - 0,10
Manganese (Mn)0,40 - 1,20
Magnesium (Mg)0,20 - 0,80
Copper (Cu)3,90 - 5,00
Titanium (Ti)0,00 - 0,15
Iron (Fe)0,00 - 0,50
Zinc (Zn)0,00 - 0,25
Nickel (Ni)0,00 - 0,10
Aluminium (Al)Balance
Physical Properties Value
Density2.80 g/cm³
Melting Point505 °C
Thermal Expansion22.8 x 10^-6 /K
Modulus of Elasticity72 GPa
Thermal Conductivity160 W/m.K
Electrical Resistivity%40 IACS
Mechanical Properties Value
Proof Strength430 MPa
Yield Strength500 MPa
Elongation A50 mm%9
Modulus of Elasticity72 GPa

High strength structural components for aircraft , military vehicles and bridges, weapons manufacture, structural applications. 

 

ALLOY DESIGNATIONS

Aluminium alloy 2014 / 2014A is covered by Standard BS EN 2100 and has similarities to the following standard designations and specifications:

2014 / 2014A, AMS 4029, ISO AlCu4SiMg, 3.1255

DIN AlCuSiMn, UNS A92014, BS L93, DTD 5010

 

TEMPER TYPES

The most common tempers for 2014 / 2014A aluminium are:

  • O   - Soft
  • T3 - Solution heat treated, cold worked and naturally aged
  • T4 - Solution heat treated and naturaly aged to a substantially stable condition
  • T6 - Solution heat treated and artificially aged
  • T651 - Solution heat treated, stress relieved by stretching then artificially aged

 

SUPPLIED FORMS

AMS 4029 aluminium is supplied in Plate.

  • Plate
DELIVERY:
Mechanical Properties
Thickness (mm) Proof Strength (Min.) Yield Strength (Min.) Elongation A50 mm %
Over 25 up to & incl. 75 415 MPa 460 MPa %7
Over 150 up to & incl. 200 350 MPa 430 MPa %6
Over 200 up to & incl. 250 320 MPa 420 MPa %5