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Aluminium Design and Construction John Dwight

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failure plane in the HAZ, close to the weld deposit, for which the<br />

limiting stress is taken as the basic parent value factored by k z1 .<br />

With welds in 7xxx material, carrying transverse tension, a check is<br />

also needed for possible failure at the dip in HAZ (point A in figure 6.2).<br />

For this we take k z =k z3 .<br />

6.7 COMPARISON WITH ONE-INCH RULE<br />

It has already been stated that the most useful HAZ treatment for general<br />

use in design is the simple, but conservative, one-inch rule. In many<br />

situations, the softened region is relatively small <strong>and</strong> any slight overestimate<br />

of its extent, through employing the one-inch rule, is justified<br />

by the simplicity. But there are other cases where HAZ effects cause a<br />

more serious drop in the resistance of a member, perhaps 10 or 20%.<br />

For these, the one-inch rule becomes too pessimistic, <strong>and</strong> something<br />

better is then needed if an economic section is to be arrived at. Our RD<br />

method is proposed as a more scientific alternative.<br />

Figure 6.18 shows two beam sections for which relevant parameters<br />

are as follows:<br />

Alloy 6082-T6<br />

Welding process MIG<br />

Limiting stress po 260 N/mm2 Softening factor kz 0.60.<br />

Included against each section is a bar-chart showing how the ratio M c /M cg<br />

varies, depending on which HAZ method is used, where M c =calculated<br />

Figure 6.18 Effect of HAZ softening on calculated resistance for two members in bending.<br />

Comparison of proposed RD method <strong>and</strong> the one-inch rule. RD method: N=normal thermal<br />

control; S=strict thermal control.<br />

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

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