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Aluminium Design and Construction John Dwight

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When the method of surface preparation does not follow the st<strong>and</strong>ard<br />

procedure, should be based on tests, which may be carried out in<br />

accordance with BS.4604: Part 1. The resulting -value may be lower or<br />

higher than 0.33, depending on the procedure used.<br />

11.2.7 Serviceability factor<br />

British St<strong>and</strong>ard BS.8118 is confusing as to the value to be used for the<br />

serviceability factor � s in equation (11.8). When the slip-factor is taken<br />

as 0.33, based on the st<strong>and</strong>ard surface preparation, alternative values<br />

� s =1.2 <strong>and</strong> 1.33 are given <strong>and</strong> it is not clear which to use when. On the<br />

other h<strong>and</strong>, when is found from tests, BS.8118 permits � s =1.1. An<br />

appropriate value would lie in the range 1.1–1.2. The value of 1.33<br />

seems too high.<br />

11.3 WELDED JOINTS<br />

11.3.1 General description<br />

In this section, we consider the static strength (ultimate limit state) of<br />

aluminium welds made by the MIG or TIG process. There are two<br />

essential differences from steel: firstly, the weld metal is often much<br />

weaker than the parent metal; <strong>and</strong>, secondly, failure may occur in the<br />

heat-affected zone (HAZ) rather than in the weld itself. The weld metal<br />

can be stronger or weaker than the HAZ material, depending on the<br />

parent/filler combination. It tends to be less ductile <strong>and</strong> better joint<br />

ductility is obtained when failure occurs in the HAZ. Refer to Chapter<br />

6 for data on HAZ softening.<br />

The various action-effects that a weld may be required to transmit,<br />

possibly occuring in combination, are as follows (Figure 11.4):<br />

(a) transverse force acting perpendicular to the axis of the weld;<br />

(b) longitudinal force acting parallel to the weld axis;<br />

(c) axial moment acting about the weld axis.<br />

Figure 11.4 Action-effects at a weld.<br />

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

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