Aluminium zinc alloy
Aluminium 7050 alloy is a heat treatable alloy. It has high toughness, high strength. It has high stress corrosion cracking resistance. [1] It has electric conductivity of value having 40 percent of copper.[2] 7050 aluminium is known as a commercial aerospace alloy.[3]
Chemical Composition
Element[1]
|
Content (%)
|
Aluminum, Al
|
89
|
Copper, Cu
|
2.3
|
Magnesium, Mg
|
2.3
|
Zinc, Zn
|
6.2
|
Zirconium, Zr
|
0.12
|
Physical Properties
Properties[1]
|
Metric
|
Density
|
2.6-2.8 g/cm3
|
Melting point
|
494°C
|
Tensile strength
|
515 MPa
|
Yield strength
|
455 MPa
|
Fatigue strength
|
240 MPa
|
Elastic modulus
|
70-80 GPa
|
Poisson's ratio
|
0.33
|
Elongation
|
11%
|
Thermal conductivity
|
180 W/mK
|
Designations
It can be written as:[1]
- AMS 4108
- AMS 4201
- ASTM B247
- ASTM B316
- QQ A-430
Welding
Welding should be avoided, because it weakens aluminum alloy. [2]
Applications
- Aircraft and other structures[1]
- Fuselage frames[2]
- Bulkheads[2]
- Wing skins[3]
- Military aircraft applications[3]
References
Further reading
External links
- For more properties, visit: http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MA7050T765
- Aluminum 7050 properties for different thickness https://www.aircraftmaterials.com/data/aluminium/7050.html
Aluminum alloy table