Aluminium alloy 6082 is a medium strength alloy with excellent corrosion resistance. It has the highest strength of the 6000 series alloys. Alloy 6082 is known as a structural alloy. In plate form, 6082 is the alloy most commonly used for machining. As a relatively new alloy, the higher strength of 6082 has seen it replace 6061 in many applications. The addition of a large amount of manganese controls the grain structure which in turn results in a stronger alloy. 6082-T651 is now superseding low-carbon steels in structural applications where the benefits of lightness, specific stiffness, corrosion resistance and ease of fabrication can be exploited
Element | Composition % |
---|---|
Silicon (Si) | 0.70 - 1.3 |
Magnesium (Mg) | 0.60 - 1.20 |
Manganese (Mn) | 0.4 - 1.00 |
Iron (Fe) | 0.0 - 0.50 |
Chromium (Cr) | 0.0 - 0.25 |
Zinc (Zn) | 0.0 - 0.20 |
Others (Total) | 0.00 - 0.15 |
Titanium (Ti) | 0.0 - 0.10 |
Copper (Cu) | 0.0 - 0.10 |
Other (Each) | 0.0 - 0.05 |
Aluminium (Al) | Balance |
Property | Value |
---|---|
Proof Stress | 260 Min MPa |
Tensile Strength | 310 MPa |
Elongation at 50 mm | 10 Min % |
Hardness Brinell | 94 HB |
Please note that Mechanical Properties shown are for T651 temper - Solution heat treated, stress relieved by stretching then artificially aged |
Property | Value |
---|---|
Density | 2.70 g/cm3 |
Melting Point | 555°C |
Thermal Expansion | 24 ×10−6 /K |
Modulus of Elasticity | 70 GPa |
Thermal Conductivity | 180 W/m.K |
Electrical Resistivity | 0.038 ×10−6Ω.m |
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