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7068

AMS 4331 / AlZn5MgCu / 7068 / T6511

Chemical Properties % Value
Silicon (Si)0,00 - 0,12
Chromium (Cr)0,00 - 0,05
Manganese (Mn)0,00 - 0,10
Magnesium (Mg)2,20 - 2,30
Copper (Cu)1,60 - 2,40
Titanium (Ti)0,00 - 0,10
Iron (Fe)0,00 - 0,15
Zinc (Zn)7,30 - 8,30
Aluminium (Al)Balance
Physical Properties Value
Density2.85 g/cm³
Melting Point476 °C
Thermal Expansion23.4 µm/m.°C
Modulus of Elasticity71.7 GPa
Thermal Conductivity190 W/m.K
Electrical Resistivity%31 IACS
Mechanical Properties Value
Proof Strength680 MPa
Yield Strength710 MPa
Shear Strength365 MPa
Elongation A50 mm%8
Hardness190 HB

7068 T6511 aluminum alloy is considered one of the strongest aluminum alloys available today and is commonly chosen by industries seeking a combination of high performance, low weight, and exceptional durability. Its applications span aircraft fuselages, defense systems, motorsport components, high-performance bicycle frames, and mold-making. Under T6 heat treatment, this alloy achieves maximum strength and hardness while maintaining lightness and robust durability.

The alloy’s surface is amenable to anodizing, which enhances both its corrosion resistance and surface hardness. However, like many high-strength aluminum alloys, 7068 T6 has limited weldability; manufacturers often opt for mechanical fastening methods such as bolts or rivets, or use specialized welding techniques when necessary. Despite its high hardness, the alloy can be bent to a limited extent if proper preheating and forming methods are employed, allowing the creation of some complex shapes and geometries.

7068 T6511 retains its structural integrity under high vibration and fatigue loads for extended periods, making it a long-lasting and reliable choice in demanding aerospace, automotive, and defense applications. Its natural corrosion resistance, further improved through appropriate surface treatments, enables the alloy to withstand harsh environmental conditions.

Its advantages include exceptional strength, light weight, superior fatigue and vibration resistance, suitability for anodizing, and good corrosion resistance. On the downside, careful machining and welding expertise are required, bending capability is restricted, and the material can be relatively expensive. These characteristics make 7068 T6511 an ideal material choice where extreme conditions and high-performance requirements are paramount.

 

ALLOY DESIGNATIONS
 
7068 T6511 has the following standard designations and specifications.

Extrusion  Rod, Flat Bar, Wire as; AMS 4331, ASTM B221  

 

Choosing Factors for 7068 T6511

  • Strength: Very good
  • Machining: Moderate
  • Weldability: Poor
  • Formability: Modarate
  • Corrosion Resistance: Good
  • Heat Treating: Yes
 
 

Some Well-Known Applications for 7068 T6511:

Critical structural components in aerospace (aircraft fuselage, wing connection elements)

High-strength and lightweight armor plates and load-bearing components in the defense industry

High-performance suspension systems, frames, and connecting elements in the automotive sector

Sports equipment (e.g., high-performance bicycle frames) and industrial machinery parts where exceptional strength-to-weight ratio is required

 

SUPPLIED FORMS
 
7068 T6511 is supplied in extruded round/flat bar.
  • Rod / Round Bar / Flat Bar
DELIVERY:
Mechanical Properties
Thickness (mm) Proof Strength (Min.) Yield Strength (Min.) Elongation A50 mm %
over 0.203 up to & incl. 0.279 430 MPa 505 MPa 5
over 0.305 up to & incl. 0.991 458 MPa 520 MPa 7
over 1.02 up to & incl. 3.17 465 MPa 535 MPa 8
over 3.20 up to & incl. 6.32 472 MPa 533 MPa 8
over 6.35 up to & incl. 12.7 459MPa 534 MPa 9
over 12.7 up to & incl. 25.4 465 MPa 538 MPa 7
over 25.43 up to & incl. 50.8 457 MPa 526 MPa 6
over 50.83 up to & incl. 63.5 437 MPa 519 MPa 5
over 63.53 up to & incl. 76.2 417 MPa 491 MPa 5
over 76.23 up to & incl. 88.9 394 MPa 485 MPa 5
over 88.93 up to & incl. 102 368 MPa 458 MPa 4