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Aluminium Design and Construction John Dwight

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Where a range is given, as for the first three elements, this denotes the<br />

minimum <strong>and</strong> maximum permitted content of an intended ingredient.<br />

Where a single figure is given (as for the last four) this refers to an<br />

impurity, which must not exceed the value quoted. This is the official<br />

way of specifying such an alloy. In everyday parlance, it is more convenient<br />

to talk in terms of the nominal composition, quoting the mean percentages<br />

of the intended elements only. The above 6082 alloy would be described<br />

as containing a nominal:<br />

Si 1.0 Mn 0.7 Mg 0.9%<br />

<strong>Aluminium</strong> alloys are grouped into seven alloy series, depending on their<br />

main alloying ingredient(s) (Table 4.1). The first digit of an alloy number<br />

indicates the series to which that alloy belongs, while the other three usually<br />

have no particular significance. An alloy series may be referred to collectively<br />

by putting xxx after the first digit, i.e. the ‘5xxx series’.<br />

Sometimes a slightly modified version of an existing alloy is registered,<br />

in which case an ‘A’ may be added to distinguish it from the original<br />

(e.g. 5154 <strong>and</strong> 5154A).<br />

The AA also carry an 8xxx series, used for compositions that do not easily<br />

fit into any of the first seven. One such type of alloy, containing a substantial<br />

amount of lithium, has raised interest in the aircraft industry because of its<br />

significantly lower density compared to other aluminium alloys.<br />

4.1.3 Work hardening<br />

Non-heat-treatable alloys are strengthened by means of cold work applied<br />

during manufacture, as in the cold reduction of sheet or drawn tube.<br />

The reduction per pass, <strong>and</strong> any heating, are controlled to produce the<br />

required combination of strength <strong>and</strong> ductility. For a given degree of<br />

cold work, the resulting increase in the proof stress (yield) is relatively<br />

much greater than the increase in tensile strength (UTS), as compared<br />

with the annealed condition.<br />

The condition (or temper) of work-hardened sheet <strong>and</strong> drawn tube can<br />

be crudely expressed in terms of its hardness, the st<strong>and</strong>ard tempers being<br />

Table 4.1 The seven alloy series<br />

Note. NHT=non-heat-treatable, HT=heat-treatable<br />

Copyright 1999 by Taylor & Francis Group. All Rights Reserved.

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