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7076

ASTM B209 / AlZn6Mg / 7076 / T61

Chemical Properties % Value
Silicon (Si)0,00 - 0,40
Chromium (Cr)0,18 - 0,28
Manganese (Mn)0,00 - 0,30
Magnesium (Mg)2,10 - 2,90
Copper (Cu)1,20 - 2,00
Titanium (Ti)0,00 - 0,20
Iron (Fe)0,00 - 0,50
Zinc (Zn)5,10 - 6,10
Aluminium (Al)Balance
Physical Properties Value
Density2.84 g/cm³
Melting Point466°C
Thermal Expansion23.2 µm/m.°C
Modulus of Elasticity71 GPa
Thermal Conductivity160 W/m.K
Electrical Resistivity%33 IACS
Mechanical Properties Value
Proof Strength470 MPa
Yield Strength510 MPa
Shear Strength310 MPa
Elongation A50 mm%14
Hardness150 HB

7076 T61 aluminum alloy stands out for its high strength, excellent fatigue resistance, and good thermal stability. As a zinc-based alloy, 7076 is widely used in aerospace, automotive, and defense industries due to its superior mechanical properties. The T61 temper indicates that the alloy has undergone solution heat treatment followed by controlled aging to enhance its strength and durability. This makes it well-suited for load-bearing structures and components operating under demanding conditions.

This alloy is commonly applied in aircraft structures, automotive frames, sports equipment, and other high-performance applications. It is compatible with anodizing, forming a protective oxide layer that improves corrosion resistance while also offering an aesthetic finish. However, due to its high zinc content, anodizing requires careful handling. The weldability of 7076 T61 is limited; its high strength can increase the risk of cracking during welding. Proper processing and the use of suitable filler materials are critical in applications requiring welding.

7076 T61 aluminum alloy has some limitations in formability due to its high strength, making complex shaping processes challenging. Nevertheless, with the right techniques, it can be successfully bent and formed for precision applications. Its exceptional fatigue resistance and mechanical stability make it ideal for use in high-vibration environments, ensuring long-term reliability in components exposed to dynamic loads.

Corrosion resistance is moderate and may require additional surface treatments or coatings when used in highly corrosive environments. Advantages of 7076 T61 include high strength, excellent fatigue resistance, and thermal stability, while its disadvantages include limited weldability, challenging formability, and moderate corrosion resistance. These characteristics make 7076 T61 an excellent material for applications requiring mechanical durability and high performance.

 

ALLOY DESIGNATIONS
 
7076 T61 has the following standard designations and specifications.

Plates per; 7076 T61, UNS A97076, ASTM B209 

 

Choosing Factors for 7076 T61

  • Strength: Excellent
  • Machining: Exceptional
  • Weldability: Fair
  • Formability: Moderate
  • Corrosion Resistance: Poor
  • Heat Treating: Yes
 

Some Well-Known Applications for 7076 T61

In propeller blades of helicopters,

In the manufacturing of engine chassis,

It is also used in the aerospace industry where high-stress is required.

 

SUPPLIED FORMS

7076 T61 is produced/supplied in the plate form.
  • Plate
DELIVERY:
Mechanical Properties
Thickness (mm) Proof Strength (Min.) Yield Strength (Min.) Elongation A50 mm %
Over 0.4 up to & incl. 12.5 145 MPa 275 MPa %10