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AA 7475 T651: High-Toughness Aluminum Alloy for Versatile Applications

AA 7475, derived from Aluminum 7075, provides excellent toughness for a broad variety of applications. This alloy offers several metalworking options that include machining, forming, and heat treating. For machining, AA 7475 functions best in the annealed condition and should be used with oil-based lubricants. It is also most easily formed in the annealed condition, as its hardened state results in spring-back. This alloy is typically available in flat rolled products, and it is widely used for applications that require high strength, including planes and other aerospace assemblies.

Properties

General

PropertyValueConditionRelated Standards

Density

2.81 g/cm³

T651

AA Standards

Mechanical

PropertyValueConditionRelated StandardsComment

Elastic modulus

70.0 GPa

T651

AA Standards

Plane-Strain Fracture Toughnes

22.0 - 35.0 MPa·√m

Typical for Wrought 7000 Series Aluminium

Poisson's ratio

0.33 [-]

Typical for Wrought 7000 Series Aluminium

Shear modulus

26.4 - 27.1 GPa

Typical for Wrought 7000 Series Aluminium

Tensile strength

585.0 MPa

T651

AA Standards

Thermal

PropertyTemperatureValueConditionRelated StandardsComment

Coefficient of thermal expansion

20 °C

2.3199999999999998e-05 1/K

T651

AA Standards

100 °C

2.3199999999999998e-05 1/K

T651

AA Standards

Melting point

475.0 - 635.0 °C

T651

AA Standards

Specific heat capacity

795.0 - 1050.0 J/(kg·K)

Typical for Wrought 7000 Series Aluminium

Thermal conductivity

138.0 - 163.0 W/(m·K)

T651

AA Standards

Electrical

PropertyValueConditionRelated Standards

Electrical conductivity

20000000.0 - 24000000.0 S/m

T651

AA Standards

Electrical resistivity

4.17e-08 - 5e-08 Ω·m

T651

AA Standards

Chemical properties

PropertyValueConditionRelated Standards

Chromium

0.18 - 0.25 %

T651

AA Standards

Copper

1.2 - 1.9 %

T651

AA Standards

Iron

0.12 %

T651

AA Standards

Magnesium

1.9 - 2.6 %

T651

AA Standards

Manganese

0.06 %

T651

AA Standards

Silicon

0.1 %

T651

AA Standards

Titanium

0.06 %

T651

AA Standards

Zinc

5.2 - 6.2 %

T651

AA Standards

Technological properties

Property
Brazing

general: no brazing is known or developed

Corrosion properties

Stress corrosion cracking: Operational damage in areas with tensile stresses transverse to the grain structure, limited damage to laboratory samples, general: good, without protection in industrial or seawater atmosphere

General machinability

General: good to acceptable

Workability

general (condition): not suitable


Metal

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