Aluminium 6082
Scope
Aluminium 6082 is a medium strength alloy with excellent corrosion resistance. It has the highest strength of 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. It is difficult to produce thin walled, complicated extrusion shapes in alloy 6082. The extruded surface finish is not as smooth as other similar strength alloys in the 6000 series. In the T6 and T651 temper, 6082 machines well and produces tight coils of swarf when chip breakers are used.
Application
This material is used for milk churns, trusses, cranes, ore skips, beer barrels, bridges, highly stressed applications and transport applications.
Supplied Forms
- Sheet
- Plate
- Extrusion
- Tube
- Bar
Alloy Designations
Aluminium alloy 6082 also corresponds to: AA6082, HE30, DIN 3.2315, EN AW-6082, ISO: Al Si1MgMn and A96082.
Temper Types
The most common tempers for 6082 aluminium are:
6063 O
Un-heat treated / Soft
6063 T4
Solution heat treated and naturally aged to a substantially stable condition
6063 T6
Solution heat treated and artificially aged
6063 T651
Solution heat treated, stress relieved by stretching then artificially aged.
Fabrication
- Solderability: Good
- Weldability - Gas: Good
- Weldability - Arc: Good
- Weldability - Resistance: Good
- Brazability: Good
- Workability - Cold: Good
- Machinability: Good
Welding
6082 has very good weldability but strength is lowered in the weld zone. When welded it itself alloy 4043 wire is recommended. If welding 6082 to 7005, then the wire used should be alloy 5356.
Chemical Compositions
Element | % Present |
---|---|
Manganese (Mn) | 0.40 - 1.00 |
Iron (Fe) | 0.00 - 0.50 |
Magnesium (Mg) | 0.60 - 1.20 |
Silicon (Si) | 0.70 - 1.30 |
Copper (Cu) | 0.00 - 0.10 |
Zinc (Zn) | 0.00 - 0.20 |
Titanium (Ti) | 0.00 - 0.10 |
Chromium (Cr) | 0.00 - 0.25 |
Aluminium (Al) | Balance |
Chemical Compositions
Element | % Present |
---|---|
Manganese (Mn) | 0.40 - 1.00 |
Iron (Fe) | 0.00 - 0.50 |
Magnesium (Mg) | 0.60 - 1.20 |
Silicon (Si) | 0.70 - 1.30 |
Copper (Cu) | 0.00 - 0.10 |
Zinc (Zn) | 0.00 - 0.20 |
Titanium (Ti) | 0.00 - 0.10 |
Chromium (Cr) | 0.00 - 0.25 |
Aluminium (Al) | Balance |
Mechanical properties at room temperature
Property | Value |
---|---|
Proof Stress | 310 MPa |
Tensile Strength | 340 MPa |
Elongation | 11% |
Shear Strength | 210 MPa |
Hardness Vickers | 100 HV |
Mechanical properties at room temperature
Property | Value |
---|---|
Proof Stress | 310 MPa |
Tensile Strength | 340 MPa |
Elongation | 11% |
Shear Strength | 210 MPa |
Hardness Vickers | 100 HV |
Reference data for some physical properties (for guidance only)
Property | Value |
---|---|
Density | 2.70 Kg/m3 |
Melting Point | 555 °C |
Thermal Expansion | 24 x 10-6 /K |
Modulus of Elasticity | 70 GPa |
Thermal Conductivity | 180W/m.K |
Electrical Resistivity | 0.038 x 10-6 Ω .m |
Reference data for some physical properties (for guidance only)
Property | Value |
---|---|
Density | 2.70 Kg/m3 |
Melting Point | 555 °C |
Thermal Expansion | 24 x 10-6 /K |
Modulus of Elasticity | 70 GPa |
Thermal Conductivity | 180W/m.K |
Electrical Resistivity | 0.038 x 10-6 Ω .m |
Editor
thyssenkrupp Materials (UK) Ltd
Cox’s Lane
Cradley Heath
West Midlands
B64 5QU
Important Note
Information given in this data sheet about the condition or usability of materials respectively products are no warranty for their properties, but act as a description. The information, we give on for advice, comply to the experiences of the manufacturer as well as our own. We cannot give warranty for the results of processing and application of the products.