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Aluminium Design and Construction John Dwight

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60 alloys, are:<br />

BSEN.485 plate <strong>and</strong> sheet;<br />

BSEN.755 extruded sections;<br />

BSEN.754 drawn tube.<br />

Figures 4.3 <strong>and</strong> 4.4 show compositions <strong>and</strong> minimum mechanical properties<br />

for a representative range of aluminium materials, mainly based on the<br />

above st<strong>and</strong>ards. Where a b<strong>and</strong> is drawn, this shows the possible range<br />

for the property concerned, depending on form <strong>and</strong> thickness.<br />

Table 4.5 presents more specific data for a shortlist of alloys, covering<br />

plate, sheet <strong>and</strong> extrusions. The strength of drawn tube can be estimated<br />

by taking that for either equivalent work-hardened sheet material, or<br />

else equivalent heat-treated extrusion material.<br />

4.3.3 Comments on certain alloys<br />

(a) 5xxx-series alloys<br />

The A-rating for durability accorded to these alloys (Table 4.4) is usually<br />

a true indication of their excellent corrosion resistance. However, when<br />

such alloys have a magnesium content higher than about 3.5 or 4%, <strong>and</strong><br />

they are required to operate in a hot environment, there is a danger of<br />

abnormal forms of corrosion (Section 4.7.1). For such applications, it is<br />

desirable to keep the magnesium content down by using a weaker<br />

alloy. For example, in the construction of welded tipper-truck bodies<br />

one would normally select one of the strongest versions of 5xxx-series<br />

alloy, such as 5083. But this alloy, with a nominal magnesium content<br />

of 4.5%, becomes unacceptable if the body has to carry hot material. In<br />

such a case, one should change to a weaker alloy with less magnesium.<br />

The following 5xxx-series alloys, not covered in Table 4.5, also appear<br />

in structural codes:<br />

5052 (Mg 2.5, Cr 0.2) slightly stronger than 5251;<br />

5754 (Mg 3.1) intermediate between 5251 <strong>and</strong> 5154A;<br />

5454 (Mg 2.7, Mn 0.7, Cr 0.1) similar strength to 5154A.<br />

(b) 6xxx-series alloys<br />

As already explained, these alloys are broadly available in a stronger <strong>and</strong><br />

a weaker version. The latter with its superb extrudability is selected when<br />

stiffness is the main criterion, the 6063 alloy being much used. For more<br />

highly stressed situations, the stronger version becomes necessary,<br />

popular alloys being 6082 in Britain, <strong>and</strong> 6061 in North America. The<br />

6061 is not quite as strong as 6082, but is slightly better for forming. Other<br />

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

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