17.11.2012 Views

Aluminium Design and Construction John Dwight

Aluminium Design and Construction John Dwight

Aluminium Design and Construction John Dwight

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Figure 4.11 Minimum stress-strain curves for a selection of aluminium materials, based on<br />

a thickness of 6 mm, generally for flat material. The 6063 curve is for 6 mm thick extruded<br />

profile.<br />

(low n). Much of aluminium construction is in materials that are either<br />

fully heat-treated, or else in a heavily work-hardened condition. These<br />

typically have a low ultimate/proof ratio (below 1.2) <strong>and</strong> hence a stressstrain<br />

curve with a fairly abrupt knee. A higher value for f u /f o ,<br />

corresponding to a more rounded curve, would be exhibited by material<br />

in the T4 or annealed condition.<br />

Figure 4.11 gives curves constructed by the above method for a selection<br />

of aluminium materials.<br />

Mazzolani discusses the use of more precise mathematical expressions<br />

for representing the stress-strain relation [26].<br />

4.5 CASTING ALLOYS<br />

Compared to forgings, castings are generally less ductile <strong>and</strong> weaker,<br />

although tensile strengths up to 300 N/mm2 are possible. They are cheaper<br />

than forgings. The design of aluminium castings is beyond the scope of<br />

this book, but below we give some limited data on certain alloys.<br />

4.5.1 Numbering system<br />

The unified system for specifying cast material, now adopted in Europe,<br />

is described in BSEN.1706. For a given material it uses a two-part reference,<br />

such as AC.51400-F or AC.42000-T6, in which the first part refers to the<br />

alloy, <strong>and</strong> the second part to the condition. In Britain, the new European<br />

alloy numbers for castings supersede the old ‘LM’ system, although the<br />

actual compositions are broadly the same.<br />

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

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!