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Aluminium Design and Construction John Dwight

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else of ingenious ‘proprietary’ design. In the late 1940s, large aluminium<br />

rivets came into use (up to 25 mm diameter), <strong>and</strong> some notable structures<br />

were built with them. High forces were needed to close these rivets <strong>and</strong><br />

special squeeze-riveters were developed for the purpose. All this<br />

disappeared with the arrival of gas-shielded arc welding in the 1950s,<br />

combined with the fact that riveting had become a lost art generally in<br />

the fabricating industry. But one wonders whether the rush to weld<br />

aluminium has not been somewhat Gadarene.<br />

Non-heat-treatable solid aluminium rivets come in 5xxx-series alloy.<br />

For the best shear strength, they should be supplied in a work-hardened<br />

condition (typically quarter-hard) <strong>and</strong> driven cold. To facilitate closing<br />

(i.e. for larger rivets), they can instead be used in the annealed Ocondition,<br />

with a slight strength penalty. In this case, they can if necessary<br />

be driven hot, the required temperature being about 350°C. Table 11.1,<br />

based on BS.8118, covers two typical rivet materials of this kind, 5154A<br />

<strong>and</strong> 5056A. The latter, which is the stronger, is not recommended for<br />

tropical environments because of possible corrosion.<br />

The alternative is to employ rivets in heat-treatable material. These<br />

are driven cold, normally in the solution-treated T4 condition. For the<br />

greatest ease of closing, they should be used within two hours of<br />

quenching, or up to four or five days if held in a refrigerator (at -6 to<br />

-10°C). Rivets of this kind would normally be in the stronger kind of<br />

6xxx-series alloy, such as 6082, for which strength data are included in<br />

Table 11.1. The British St<strong>and</strong>ard also includes data for rivets in the T6<br />

condition.<br />

<strong>Aluminium</strong> rivets should always be used in reamed holes, as they<br />

will not tolerate a bad hole in the way that hot-driven steel rivets used<br />

to. Because they are driven cold, or at a fairly modest temperature, they<br />

exert negligible clamping action between the plates. On the other h<strong>and</strong>,<br />

after driving, they fill the hole well. <strong>Aluminium</strong> rivets should not be<br />

used in situations where they have to carry tensile loading.<br />

The above information refers to conventional solid rivets, In the<br />

attachment of sheet metal panels much use is made of proprietary<br />

fasteners, which are easy to use <strong>and</strong> which are suitable for blind riveting<br />

(access to only side of the joint). Examples of these are the well-known<br />

‘pop’ <strong>and</strong> ‘chobert’ rivets, both of tubular form. Pop-rivets come in<br />

diameters up to about 5 mm. They can exert a limited clamping action,<br />

provided care is taken with plate fit-up during closing, but they do not<br />

fill the hole so well as a cold-driven solid rivet. In contrast, the chobert<br />

rivet, which is available in larger sizes, fills the hole well but has negligible<br />

clamping action. A wide range of other proprietary fasteners is available,<br />

generally more expensive, mostly for use in the aero-industry. In the<br />

USA such fasteners, which are a cross between a bolt <strong>and</strong> a rivet, are<br />

also popular in non-aeronautical construction.<br />

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

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