2618A - a strong aluminium alloy containing nominally 2% copper and 1.5% magnesium.
The alloy is produced as bar, plate, tube and is also available as clad sheet and strip. Solution treated and artificially aged to achieve the T6 condition or with the addition of controlled stretching to achieve the T6511 temper. 2618A can be employed to a maximum of 300°C and retains mechanical strength relatively well to around 200°C and above. The alloy has a density of 2.75 g/cc.
- Aerospace Equivalent (bar) - DTD 5014A
- General Engineering Euronorm - EN 573 EN AW-2618A (composition) (AlCu2Mg1.5Ni)
- Old BS (pre-1980) Specification - H16
Application
- Aerospace & Defence Components
- High Technology Applications
Features
- Extremely high strength
- Good machinabilit
- Fair resistance to atmospheric attack
Specification
MOQ：3Ton
Stay Connect