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2014 clad

AIR 9048.090 / AlCu4SiMg / 2014 clad / T6

Chemical Properties % Value
Silicon (Si)0,5 - 1,2
Chromium (Cr)0,00 - 0,10
Manganese (Mn)0,40 - 1,20
Magnesium (Mg)0,20 - 0,80
Copper (Cu)0,00 - 0,70
Titanium (Ti)0,00 - 0,15
Iron (Fe)0,00 - 0,70
Zinc (Zn)0,00 - 0,25
Aluminium (Al)Balance
Physical Properties Value
Density2.8 g/cm³
Melting Point507 °C
Thermal Expansion22.7 µm/m°C
Modulus of Elasticity72 GPa
Thermal Conductivity130 W/m.K
Electrical Resistivity40 % IACS
Mechanical Properties Value
Proof Strength420 MPa
Yield Strength490 MPa
Shear Strength290 MPa
Elongation A50 mm6.8 %
Hardness140 HB
2014 Clad T6 Temperature – Ultimate Tensile Strength Graph
2014 Clad T6 Temperature – Ultimate Tensile Strength Graph
2014 Clad T6 Thickness – Ultimate Tensile Strength Graph
2014 Clad T6 Thickness – Ultimate Tensile Strength Graph
2014 Clad T6 Diameter – Ultimate Tensile Strength Graph
2014 Clad T6 Diameter – Ultimate Tensile Strength Graph
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The 2014 clad T6 aluminum alloy is a member of the Al-Cu (Aluminum-Copper) alloy series widely used in engineering applications that require high strength. The T6 temper is achieved through solution heat treatment followed by artificial aging, which gives the alloy very high mechanical properties. The “clad” layer refers to a thin coating of pure aluminum on the surface, which significantly improves corrosion resistance. This feature is particularly important for structural components used in aerospace and defense industries.

The 2014-T6 clad alloy is known for its high tensile strength and yield strength. In terms of strength, it provides higher performance than 6061-T6 aluminum alloy and can approach the mechanical strength of 7075-T6 alloy. However, compared to 7075 alloy, it offers better machinability and a more balanced mechanical response. Its high strength-to-weight ratio makes it a preferred material for load-bearing structural components.

In terms of machinability, 2014 clad T6 alloy demonstrates excellent machining performance despite its relatively high copper content. This makes it widely used in the production of precision components. However, its bending and forming capability is limited, especially in the T6 temper condition, and forming operations are usually performed in softer temper states. Nevertheless, when proper processing parameters are used, the alloy can provide good surface quality and dimensional accuracy.

Regarding coatings and surface treatments, 2014 clad alloy provides a suitable base for anodizing and other surface finishing processes. It also exhibits good fatigue resistance under vibration and cyclic loads, which makes it suitable for aircraft structures and mechanical components operating in high-vibration environments. However, its weldability is limited, and in many applications riveting or mechanical fastening methods are preferred.

This alloy is widely used in aerospace, defense, machinery manufacturing, and high-performance engineering sectors. Aircraft structural components, fittings, plates, and high-strength mechanical parts are among its most common applications. While it belongs to a similar strength class as the 2024 alloy, it provides higher strength than 6061 and in some applications offers better machinability and cost balance compared to the 7075 alloy.

 

STANDARDS OF MATERIAL CHEMICAL COMPOSITION

2014 T6 clad may comply with the following standards.
• 2014 T6 Alclad Sheet; AMS QQ-A-250/3, ASTM B209,ISO AlCu4SiMg, UNS A92014,BS L 165, AIR 9048.090, EN 2087

 

Characteristics for 2014 T6 clad: 

  • Strength: Excellent
  • Machinability: Very good
  • Weldability: Poor (build-up welding is the best option)
  • Formability: Good
  • Corrosion Resistance: Low (Improved by cladding)
  • Heat Treatment: Yes
     

Some widely known application areas of 2014 T6 clad: 
High-strength structural materials,
Automotive industry and military vehicle manufacturing,
Bridge construction and the aerospace sector.

 

STOCK
We carry out the production/supply of 2014 T6 clad in sheet form.

  • Sheet
DELIVERY:
Mechanical Properties
Thickness (mm) Proof Strength (Min.) Yield Strength (Min.) Elongation A50 mm %
Over 1.02 up to & incl. 6.32 414 MPa 469 MPa %8
Over 6.35 up to & incl. 12.7 395 MPa 440 MPa %10