Aluminum alloys

2219

Spécifications

EU
Al Cu6Mn
USA
UNS: A92219
ISO Symbol
Al Cu6Mn

Composition

V
0.1
Mn
0.3
Ti
0.06
Al
Base
Cu
6.3
Mg
0.18

Applications

• Supersonic aircraft structures and space industry applications.

Characteristics

• High toughness.
• In the T8 condition (cold worked and aged), this alloy has excellent stress corrosion resistance.
• Weldable.

Mechanical properties

Heat
treatment
UTS
(N/mm²)
0,2%
YS
(N/mm²)
A
(%)
T6 condition thickness < 100 mm > 400 > 276 > 5
T851 - T852 - T854 conditions thickness 100/200 mm> 395> 300> 6

Key to heat treatment symbols

Solution treated H Annealed R
Thermo-mechanical treatment TM Quenched and tempered T+RV
Sub-zero treatment F Solution treated and aged H+V

See also

5083

Aluminum alloys