7020
Grade 7020 is a heat treatable aluminium alloy with zinc added as the main alloying element. This enhances the mechanical property attributes of the material and increases its resistance to fatigue stress.
The 7020 grade is primarily used in aerospace applications and offers a reasonable machinability. As a result the surface finish allows the material to be protective anodised but it will not lend itself to aesthetic anodising.
Forming and machining of aluminium / aluminum 7020 alloy is good. Welding, aesthetic anodizing and brazing or soldering is not suitable; however protective anodizing can be performed if required.
Chemical Composition
Aluminium |
Rem |
Silicon |
0.35% max |
Copper |
0.20% max |
Iron |
0.40% max |
Manganese |
0.05-0.50% |
Magnesium |
1.0-1.4% |
Zinc |
4.0-5.0% |
Zirconium |
0.08-0.20% |
Chromium |
0.10-0.35% |
Zirconium + Titanium |
0.08-0.25% |
Total Others |
0.15% max |
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Related Specifications
BS4300/15 |
AZ5G |
UNS: A97020 |
BS H17 |
EN AW-7020 |
Al Zn4.5Mg1 |
DIN W/S 3.4335 |
BA 733 |
Key Features
- Very good Mechanical Strengths
- Good resistance to fatigue strength.
- Good Machinability
Typical Physical Properties
Density |
2.78 g/cm³ |
Thermal conductivity |
134 W/m°K |
Thermal expansion coefficient |
23.1 x 10-6 |
Electrical Conductivity |
37.5 IACS |
Electrical resistivity |
0.046 microhm m |
Modulus of elasticity |
68 GPa |
Fabrication Properties
Cold Formability |
Good |
Machinability |
Good |
Weldability |
This grade is weldable but for more details contact the HD technical department. |
Typical Applications
Grade 7020 is generally used in aerospace applications and for radiator and heat exchanger components.
This technical information is given by Holme Dodsworth Metals without charge and the user shall employ such information at their own discretion and risk. For more detailed technical advice on temper selection, fabrication, joining, machining, physical and mechanical data please contact us as space does not permit the listing of every feature of the material.