Specification :
Designation of Aluminium
Aluminium is most commonly alloyed with copper, zinc, magnesium, silicon,
manganese and lithium. Small additions of chromium, titanium, zirconium, lead, bismuth and nickel are also made and iron is
invariably present in small quantities. There are over 300 wrought alloys with 50 in common use. They are normally identified by a four figure system
which originated in the USA and is now universally accepted. Following Table describes the system for wrought alloys. Cast alloys have similar designations and use a five
digit system.
Alloying Element
|
Alloy Series
|
None (99%+ Aluminium)
|
1XXX
|
Copper
|
2XXX
|
Manganese
|
3XXX
|
Silicon
|
4XXX
|
Magnesium
|
5XXX
|
Magnesium + Silicon
|
6XXX
|
Zinc
|
7XXX
|
Lithium
|
8XXX
|
For unalloyed wrought aluminium alloys designated 1XXX, the last two digits represent the purity of the
metal. They are the equivalent to the last two digits after the decimal point when aluminium purity is expressed to the nearest 0.01 percent. The second
digit indicates modifications in impurity limits. If the second digit is zero, it indicates unalloyed aluminim having natural impurity limits and 1 through 9, indicate
individual impurities or alloying elements.
For the 2XXX to 8XXX groups, the last two digits identify different aluminium alloys in the group. The second digit indicates alloy
modifications. A second digit of zero indicates the original alloy and integers 1 to 9 indicate consecutive alloy modifications.
Heat Treatment
A
range of heat treatments can be applied to aluminium alloys.
·
Homogenisation
– the removal of segregation by heating after casting.
·
Annealing – used
after cold working to soften work-hardening alloys (1XXX, 3XXX and 5XXX).
·
Precipitation or
age hardening (alloys 2XXX, 6XXX and 7XXX).
·
Solution heat
treatment before ageing of precipitation hardening alloys.
·
After
heat treatment a suffix is added to the designation numbers.
The suffix F means “as fabricated”.
O means “annealed
wrought products”.
T means that it
has been “heat treated”.
W means the
material has been solution heat treated.
H refers to non
heat treatable alloys that are “cold worked” or “strain hardened”.
The
non-heat treatable alloys are those in the 3XXX, 4XXX and 5XXX
groups.
Temper
|
Description of process for Heat
Treatable alloys
|
T1
|
Cooled from an elevated temperature shaping process and
naturally aged.
|
T2
|
Cooled from an elevated temperature shaping process cold
worked and naturally aged.
|
T3
|
Solution heat-treated cold worked and naturally aged to a
substantially.
|
T4
|
Solution heat-treated and naturally aged to a substantially
stable condition.
|
T5
|
Cooled from an elevated temperature shaping process and then
artificially aged.
|
T6
|
Solution heat-treated and then artificially aged.
|
T7
|
Solution heat-treated and overaged/stabilised.
|
Work
Hardening
The
non-heat treatable alloys can have their properties adjusted by cold
working. Cold rolling is a typical example.
These
adjusted properties depend upon the degree of cold work and whether
working is followed by any annealing or stabilising thermal
treatment.
Nomenclature to describe these treatments uses a letter, O, F or H
followed by one or more numbers. As outlined in Table 3, the first
number refers to the worked condition and the second number the
degree of tempering.
Hardness
|
Description of Process
for Non-Heat Treatable alloys
|
H1X
|
Work hardened
|
H2X
|
Work hardened and partially annealed
|
H3X
|
Work hardened and stabilized by low temperature treatment
|
H4X
|
Work hardened and stoved
|
HX2
|
Quarter-hard – degree of working
|
HX4
|
Half-hard – degree of working
|
HX6
|
Three-quarter hard – degree of working
|
HX8
|
Full-hard – degree of working
|
Temper codes for plate
Hardness
|
Description of Process
|
H112
|
Alloys that have some tempering from shaping but do not have
special control over the amount of strain-hardening or
thermal treatment. Some strength limits apply.
|
H321
|
Strain hardened to an amount less than required for a
controlled H32 temper.
|
H323
|
A version of H32 that has been hardened to provide
acceptable resistance to stress corrosion cracking.
|
H343
|
A version of H34 that has been hardened to provide
acceptable resistance to stress corrosion cracking.
|
H115
|
Armour plate.
|
H116
|
Special corrosion-resistant temper.
|
|