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KAISER ALUMINUM TECHNICAL REFERENCE
LIBRARY No. 1012
Aluminum Alloys, Tempers and
Terminology
| Alloy Designation
System |
A system for designating
wrought aluminum and wrought aluminum alloys was established by the Aluminum Association.
Specific limits for chemical composition to which conformance is required are provided by
applicable product standards. |
| Wrought Aluminum and Aluminum Alloy Designation System |
A system of four-digit
numerical designations is used to identify wrought aluminum and wrought aluminum alloys.
The first digit indicates the alloy group as
follows:
|
Aluminum, 99.00% minimum and greater |
1XXX |
Aluminum alloys grouped by major alloying elements
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Copper (Cu). |
2XXX |
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Manganese (Mn) |
3XXX |
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Silicon (Si) |
4XXX |
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Magnesium (Mg) |
5XXX |
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Magnesium and Silicon (Mg and Si) |
6XXX |
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Zinc (Zn) |
7XXX |
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Other elements |
8XXX |
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Unused series |
9XXX |
| Pure Aluminum |
| In the 1XXX group for minimum aluminum purities of 99.00 percent
and greater, the last two of the four digits in the designation indicate the minimum
aluminum percentage. These digits are the same as the last two digits to the right of the
decimal point in the minimum aluminum percentage when it is expressed to the nearest 0.01
percent. The second digit in the designation indicates modifications in impurity limits.
If the second digit is zero, it indicates unalloyed aluminum having natural impurity
limits; integers 1 through 9, which are assigned consecutively as needed, indicate special
control of the of more individual impurities or alloying elements. |
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| Aluminum Alloys |
| In the 2XXX through 8XXX alloy groups the last two of the four
digits in the designation have no special significance but serve only to identify the
different aluminum alloys in group. The second digit in the alloy designation indicates
alloy modifications. If the second digit is zero, it indicates the original alloy;
integers 1 through 9, which are assigned consecutively, indicate alloy modifications. |
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| Temper
Designation System |
| The temper designation system is
used for all forms of wrought and cast aluminum and aluminum alloys except ingot. It is
based on the sequence of basic treatments used to produce various tempers. The temper
designation follows the alloy designation with the two separated by a hyphen. Basic
designations consist of a letter while subdivisions of those basic tempers, where
required, are indicated by one or more digits following those letters. The system is
designed to set down specific sequences of fabrication processes, but only those
operations that are recognized as significantly influencing the characteristics of the
product involved. Should some other variation of the same sequence of basic operations be
applied to the same alloy, resulting in different characteristics, the additional digits
will be added to the numerical designation. |
| Basic
Temper Designations |
| F |
as fabricated. Denotes
metal that has been fabricated to ordered dimensions without any attempt on the part of
the producer to control the results of either strain-hardening operations or thermal
treatments. There are no mechanical property limits, and the strength levels may vary form
lot to lot and from shipment to shipment. |
| O |
annealed. Applies to wrought products
that have undergone a thermal treatment to reduce their mechanical property levels to
their minimums. Often described as "dead soft" metal. |
| W |
solution heat-treated. An unstable temper
applying to certain of the (7XXX) heat-treatable alloys that, after heat treatment,
spontaneously age harden at room temperature. Only when the period of natural aging is
indicated (W 1hr. for example) is this a specific and complete designation. |
| H |
strain-hardened. Applies to those wrought
products which have had an increase in strength by reduction through strain-hardening or
cold working operations. The "H" is always followed by two or more digits. |
| T |
thermally treated to produce tempers other than F, O or
H. Applies to those products which have had an increase in strength due to
thermal treatments, with or without supplementary strain-hardening operations. The
"T" is always followed by one or more digits. |
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| Subdivisions of
"T" Temper- |
| Heat-Treatable Alloys |
| T1 |
cooled from an elevated temperature shaping
process and naturally aged to a substantially stable condition. Usually
associated with extruded products and limited to the 6XXX series alloys. |
| T2 |
cooled from an elevated temperature shaping
process, cold worked, and naturally aged to a substantially stable condition. Usually
associated with cast products. |
| T3 |
solution heat-treated, cold worked, and
naturally aged to a substantially stable condition. (T4+cold work) |
| T4 |
solution heat-treated, and naturally aged
to a substantially stable condition. |
| T5 |
cooled from an elevated temperature shaping
process and artificially aged. Usually associated with extruded products in
the 6XXX series alloys. (T1+artificial age) |
| T6 |
solution heat-treated, and artificially
aged. (T4+artificial age) |
| T7 |
solution heat-treated, and
overaged/stabilized. Applies to alloy products which are thermally overaged
after solution heat-treatment to carry them beyond the point of maximum strength to
provide control of some special characteristic. |
| T8 |
solution heat-treated, cold worked, and
artificially aged. (T3+artificial age) |
| T9 |
solution heat-treated, artificially aged
and cold worked. (T6+artificial age) |
| T10 |
cooled from an elevated temperature shaping
process, cold worked, and artificially aged. Usually associated with cast
products.(T2+artificial age) |
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| The following specific digits have
been assigned for stress-relieved tempers of wrought products: |
| T_51 |
Applies to cold finished rod or bar when
stress-relieved by stretching 1 to 3 % permanent set. Stretching is performed after
solution heat treatment or after cooling from an elevated temperature shaping process. No
straightening takes place after stretching. |
| T_510 |
Applies to extruded products and to drawn tube when
stress-relieved by stretching 1 to 3 % permanent set. Stretching is performed after
solution heat treatment or after cooling from an elevated temperature shaping process. No
straightening takes place after stretching 1 to 3 % permanent set. |
| T_511 |
Applies to extruded products and to drawn tube when
stress-relieved by stretching 1 to 3 % permanent set. Stretching is performed after
solution heat treatment or after cooling from an elevated temperature shaping process.
These products may receive minor straightening after stretching to comply with standard
tolerances. |
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| Subdivisions of
"H" Temper- |
| Non-Heat-Treatable
Alloys |
| H1 |
strain-hardened only. Applies
to products which are strain-hardened or cold worked to obtain the desired strength level
without supplementary thermal treatments. The number following this designation indicates
the degree of strain-hardening. |
| H2 |
strain-hardened partially annealed. Applies
to products strain-hardened or cold worked more than the desired level by partial
annealing. The number following this designation indicates the degree of strain hardening
remaining after the partial annealing process. |
| H3 |
strain-hardened and stabilized. Applies
to products in the magnesium-aluminum class which will age-soften at room temperature
after strain-hardening. These products are strain-hardened to the desired amount and then
subjected to a low temperature thermal operation which results in a improved ductility.
The number following this designation indicates the degree of strain-hardening remaining
after the stabilization treatment. |
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The digit following the
designation H1, H2 or H3 indicates the degree of strain-hardening s follows:
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H_1 |
1/8 hard |
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H_2 |
1/4 hard |
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H_3 |
3/8 hard |
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H_4 |
1/2 hard |
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H_5 |
5/8 hard |
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H_6 |
3/4 hard |
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H_7 |
7/8 hard |
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H_8 |
full hard (approximately 75% reduction after a full
anneal). |
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H_9 |
extra hard (limited to certain alloys and/or product
forms). |
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