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Aluminium is the world’s most abundant metal
and is the third most common element comprising 8% of the earth’s crust. The
versatility of aluminium makes it the most widely used
metal after steel.
Production of
Aluminium
Aluminium is derived from the mineral
bauxite. Bauxite is converted to aluminium oxide (alumina) via the Bayer
Process. The alumina is then converted to aluminium metal using electrolytic cells and
the Hall-Heroult Process.
Annual Demand of
Aluminium
Worldwide demand for aluminium is around 29 million tons per
year. About 22 million tons is new aluminium and 7 million tons is recycled aluminium scrap. The use of recycled aluminium is economically and
environmentally compelling. It takes 14,000 kWh to produce 1 tonne of new aluminium. Conversely it takes only 5% of
this to remelt and recycle one tonne of aluminium. There is no difference in quality
between virgin and recycled aluminium alloys.
Applications of
Aluminium
Pure aluminium is soft, ductile, corrosion
resistant and has a high electrical conductivity. It is widely used for foil and
conductor cables, but alloying with other elements is necessary to provide the
higher strengths needed for other applications. Aluminium is one of the lightest engineering
metals, having a strength to weight ratio superior to steel.
By utilising various combinations of its advantageous
properties such as strength, lightness, corrosion resistance, recyclability and
formability, aluminium is being employed in an
ever-increasing number of applications. This array of products ranges from
structural materials through to thin packaging foils.
Alloy Designations
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. Table 1 describes the system for wrought alloys.
Cast alloys have similar designations and use a five digit system.
Table 1. Designations for wrought aluminium alloys.
|
Alloying Element |
Wrought |
|
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 aluminium 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.
Physical Properties of
Aluminium
Density of
Aluminium
Aluminium has a density around one third
that of steel or copper making it one of the lightest commercially available
metals. The resultant high strength to weight ratio makes it an important
structural material allowing increased payloads or fuel savings for transport
industries in particular.
Strength of
Aluminium
Pure aluminium doesn’t have a high tensile
strength. However, the addition of alloying elements like manganese, silicon,
copper and magnesium can increase the strength properties of aluminium and produce an alloy with
properties tailored to particular applications.
Aluminium is well suited to cold
environments. It has the advantage over steel in that its’ tensile strength
increases with decreasing temperature while retaining its toughness. Steel on
the other hand becomes brittle at low temperatures.
Corrosion Resistance of
Aluminium
When exposed to air, a layer of aluminium oxide forms almost instantaneously
on the surface of aluminium. This layer has excellent
resistance to corrosion. It is fairly resistant to most acids but less resistant
to alkalis.
Thermal Conductivity of
Aluminium
The thermal conductivity of aluminium is about three times greater than
that of steel. This makes aluminium an important material for both
cooling and heating applications such as heat-exchangers. Combined with it being
non-toxic this property means aluminium is used extensively in cooking
utensils and kitchenware.
Electrical Conductivity of
Aluminium
Along with copper, aluminium has an electrical conductivity
high enough for use as an electrical conductor. Although the conductivity of the
commonly used conducting alloy (1350) is only around 62% of annealed copper, it
is only one third the weight and can therefore conduct twice as much electricity
when compared with copper of the same weight.
Reflectivity of
Aluminium
From UV to infra-red, aluminium is an excellent reflector of
radiant energy. Visible light reflectivity of around 80% means it is widely used
in light fixtures. The same properties of reflectivity makes aluminium ideal as an insulating material to
protect against the sun’s rays
in summer, while insulating against heat loss in winter.
Table 2. Typical properties for aluminium.
|
Property |
Value |
|
Atomic
Number |
13 |
|
Atomic Weight
(g/mol) |
26.98 |
|
Valency |
3 |
|
Crystal
Structure |
FCC |
|
Melting Point
(°C) |
660.2 |
|
Boiling Point
(°C) |
2480 |
|
Mean Specific Heat (0-100°C)
(cal/g.°C) |
0.219 |
|
Thermal Conductivity
(0-100°C) (cal/cms. °C) |
0.57 |
|
Co-Efficient of Linear
Expansion (0-100°C) (x10-6/°C) |
23.5 |
|
Electrical Resistivity at
20°C (Ω.cm) |
2.69 |
|
Density
(g/cm3) |
2.6898 |
|
Modulus of Elasticity
(GPa) |
68.3 |
|
Poissons
Ratio |
0.34 |
Mechanical Properties of
Aluminium
Aluminium can be severely deformed without
failure. This allows aluminium to be formed by rolling,
extruding, drawing, machining and other mechanical processes. It can also be
cast to a high tolerance.
Alloying, cold working and heat-treating can all be utilised
to tailor the properties of aluminium.
The tensile strength of pure aluminium is around 90 MPa but this can be
increased to over 690 MPa for some heat-treatable alloys.
Table 3.
Mechanical properties of selected aluminium alloys.
|
Alloy |
Temper |
Proof Stress 0.2% (MPa) |
Tensile Strength (MPa) |
Shear Strength (MPa) |
Elongation A5 (%) |
Hardness Vickers (HV) |
|
AA1050A |
H12
H14
H16
H18
0 |
85
105
120
140
35 |
100
115
130
150
80 |
60
70
80
85
50 |
12
10
7
6
42 |
30
36
-
44
20 |
|
AA2011 |
T3
T6 |
290
300 |
365
395 |
220
235 |
15
12 |
100
115 |
|
AA3103 |
H14
0 |
140
45 |
155
105 |
90
70 |
9
29 |
46
29 |
|
AA4015 |
0
H12
H14
H16
H18 |
45
110
135
155
180 |
110-150
135-175
160-200
185-225
210-250 |
-
-
-
-
- |
20
4
3
2
2 |
30-40
45-55
-
-
- |
|
AA5083 |
H32
0/H111 |
240
145 |
330
300 |
185
175 |
17
23 |
95
75 |
|
AA5251 |
H22
H24
H26
0 |
165
190
215
80 |
210
230
255
180 |
125
135
145
115 |
14
13
9
26 |
65
70
75
46 |
|
AA5754 |
H22
H24
H26
0 |
185
215
245
100 |
245
270
290
215 |
150
160
170
140 |
15
14
10
25 |
75
80
85
55 |
|
AA6063 |
0
T4
T6 |
50
90
210 |
100
160
245 |
70
11
150 |
27
21
14 |
85
50
80 |
|
AA6082 |
0
T4
T6 |
60
170
310 |
130
260
340 |
85
170
210 |
27
19
11 |
35
75
100 |
|
AA6262 |
T6
T9 |
240
330 |
290
360 |
-
- |
8
3 |
-
- |
|
AA7075 |
0
T6 |
105-145
435-505 |
225-275
510-570 |
150
350 |
9
5 |
65
160 |
Aluminium Standards
The old BS1470 standard has been replaced by nine EN
standards. The EN standards are given in table 4.
Table 4. EN standards for aluminium
|
Standard |
Scope |
|
EN485-1 |
Technical conditions for
inspection and delivery |
|
EN485-2 |
Mechanical
properties |
|
EN485-3 |
Tolerances for hot rolled
material |
|
EN485-4 |
Tolerances for cold rolled
material |
|
EN515 |
Temper
designations |
|
EN573-1 |
Numerical alloy designation
system |
|
EN573-2 |
Chemical symbol designation
system |
|
EN573-3 |
Chemical
compositions |
|
EN573-4 |
Product forms in different
alloys |
The EN standards differ from the old standard, BS1470 in the
following areas:
·
Chemical compositions – unchanged.
·
Alloy numbering system – unchanged.
·
Temper designations for heat treatable alloys now cover a wider
range of special tempers. Up to four digits after the T have been introduced for
non-standard applications (e.g. T6151).
·
Temper designations for non heat treatable alloys – existing
tempers are unchanged but tempers are now more comprehensively defined in terms
of how they are created. Soft (O) temper is now H111 and an intermediate temper
H112 has been introduced. For alloy 5251 tempers are now shown as
H32/H34/H36/H38 (equivalent to H22/H24, etc). H19/H22 & H24 are now shown
separately.
·
Mechanical properties – remain similar to previous figures. 0.2%
Proof Stress must now be quoted on test certificates.
·
Tolerances have been tightened to various degrees.
Heat Treatment
of
Aluminium
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.
·
Stoving for the curing of coatings
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.
Table 5. Heat
treatment designations for aluminium and aluminium alloys.
|
Term |
Description |
|
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
of
Aluminium
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 6, the first number
refers to the worked condition and the second number the degree of
tempering.
Table 6.
Non-Heat treatable alloy designations
|
Term |
Description |
|
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 |
Table 7.
Temper codes for plate
|
Code |
Description |
|
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. |
|