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Aluminium Design and Construction John Dwight

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the softening is the famous ‘one-inch rule’ which often proves adequate,<br />

but not always [18]. This simple method is explained in Section 6.5.3,<br />

after which we go on to present a more scientific treatment (RD method),<br />

which may be used to replace the one-inch rule in situations that dem<strong>and</strong><br />

a more accurate estimate of the HAZ extent (Sections 6.5.4–6.5.11).<br />

Many people think that HAZ softening is such a minor effect that a<br />

very rough estimate of its extent is all that is needed. It is true that with<br />

large multi-pass welds, as used in massive members, the softened area<br />

only extends a short distance in relation to the size of the weld. For<br />

these, almost any extent-rule will usually do. But with smaller welds,<br />

as used in thin members, the extent of the HAZ is relatively much<br />

greater <strong>and</strong> a better approach is desirable. For these, the one-inch rule<br />

can lead to an estimate of member resistance that is unacceptably low.<br />

The BS.8118 procedure for predicting HAZ extent gets the worst of<br />

both worlds, since it is more awkward to apply than the one-inch rule<br />

<strong>and</strong> often inaccurate. Our proposed method is more realistic, although<br />

still fairly approximate compared to most structural calculations. In<br />

recent years, special computer programs have become available, which<br />

accurately model the temperature changes during welding <strong>and</strong> the<br />

resulting metallurgical effect [19]. For a mass-produced component, it<br />

may be sensible to employ one of these. Alternatively, the HAZ pattern<br />

can be found experimentally by making a hardness survey on a prototype.<br />

<strong>Design</strong>ers should also be aware of the locked-in (‘residual’) stresses<br />

in welded components, even though these are not directly considered<br />

in the design process. As with steel, there is a region of locked-in<br />

longitudinal tensile stress at any weld, balanced by compressive stresses<br />

elsewhere in the section. But compared to steel, where the tensile stress<br />

at the weld is invariably up to yield, the stress levels in aluminium are<br />

relatively low. The zone of locked-in longitudinal tension at an aluminium<br />

weld is generally narrower than the HAZ. Mazzolani provides interesting<br />

plots of residual stress in welded aluminium members [26].<br />

Most of this chapter specifically covers HAZ softening at welds<br />

made by the MIG process. TIG welds, for which the HAZ effects are<br />

much less predictable, are considered in Section 6.8. The friction-stir<br />

process is still very new, but some preliminary results suggest that the<br />

softening at FS welds will tend to be less extensive than that at arc<br />

welds (Section 6.9).<br />

6.2 THERMAL CONTROL<br />

The extent of the HAZ can be critically affected by the control of<br />

temperature during fabrication. In a large multi-pass joint, if no such<br />

control were exercised, the temperature of the surrounding metal would<br />

just keep on rising as more passes were laid, leading to a vastly enlarged<br />

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

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