home  |  contact  |  specification |  properties |  standard |  environment  |  technical
link one
link two
link three
link four
link five
link six
link seven
link eight


      Physical Properties

      Mechanical Properties

      Chemical Properties
 

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.