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Aluminium Design and Construction John Dwight

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softening in the heat-affected zone. Broadly they divide into a stronger<br />

type <strong>and</strong> a weaker type.<br />

The stronger type of 6xxx material in the T6 condition is sometimes<br />

described as the ‘mild steel’ of aluminium, because it is the natural<br />

choice for stressed members. In fact it is a weaker material than mild<br />

steel, with a similar proof or yield stress (250 N/mm 2 ), but a much<br />

lower tensile strength (300 N/mm 2 ). It is also less ductile.<br />

The weaker type of 6xxx alloy, which is not normally offered as sheet or<br />

plate, is the extrusion alloy par excellence. It is more suitable than any other<br />

alloy for the extrusion of thin difficult sections, <strong>and</strong> is a common choice for<br />

members that operate at a relatively low stress level, especially when good<br />

surface finish is important. Typical examples are when design is governed<br />

by stiffness (rather than strength) as with many architectural members, or<br />

when fatigue is critical, as for example in the structure of railcars.<br />

(c) 7xxx-series alloys<br />

These alloys mainly contain zinc <strong>and</strong> magnesium. Like the 6xxx-series,<br />

they can be either of a stronger or a weaker type. The stronger type<br />

embraces the strongest of all the aluminium alloys, with tensile strengths<br />

in the T6 condition up to 550 N/mm2 . The application of such alloys is<br />

almost entirely in aircraft. They have inferior corrosion resistance, poor<br />

extrudability <strong>and</strong> are unsuitable for arc welding. As with 2xxx alloys,<br />

sheet can be supplied in clad form to prevent corrosion (Section 2.2.5).<br />

The weaker type of 7xxx material is a very different proposition <strong>and</strong><br />

in the non-aeronautical field is a valid alternative to the stronger type<br />

of 6xxx material, especially for welded construction. It has superior<br />

mechanical properties to 6xxx material, <strong>and</strong> HAZ softening at welds is<br />

less severe. But corrosion resistance, although much better than for the<br />

stronger kind of 7xxx alloy, is not as good as with 6xxx alloy. Also there<br />

can be a possibility of stress-corrosion. Extrudability is not quite as<br />

good as for the 6xxx series, but hollow (bridge-die) extrusions are still<br />

possible. An important factor, when using 7xxx-series alloy as against<br />

6xxx alloy, is the need for greater expertise in fabrication.<br />

4.3 DATA ON SELECTED WROUGHT ALLOYS<br />

4.3.1 How mechanical properties are specified<br />

<strong>Aluminium</strong> material st<strong>and</strong>ards quote two levels of stress, both of which<br />

must be attained for a batch of material to be accepted:<br />

fo fu minimum value of the 0.2% proof stress (or ‘0.2% offset’);<br />

minimum tensile strength (or ‘ultimate stress’).<br />

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

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