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aluminium in commercial vehicles - European Aluminium Association

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78 EUROPEAN ALUMINIUM ASSOCIATION ALUMINIUM IN COMMERCIAL VEHICLES CHAPTER VI<br />

The properties of the parent<br />

material have very little <strong>in</strong>fluence<br />

on the fatigue strength <strong>in</strong> practi-<br />

cal structures and components.<br />

For connections the properties of<br />

the parent material have no<br />

S<br />

Δσ<br />

Δσ C<br />

Δσ D<br />

Δσ L<br />

2)<br />

1) Number of cycles (108 ) at<br />

which the cut-off limit is def<strong>in</strong>ed<br />

2) For low cycles fatigue, this<br />

part of the curve may not be cor-<br />

1<br />

b<br />

<strong>in</strong>fluence at all. For a plate or<br />

extrusion with no manufactur<strong>in</strong>g<br />

or only holes and notches the<br />

standard deviate between EN<br />

AW 7020 and all other structural<br />

alloys.<br />

‰<br />

m 1<br />

a<br />

N C<br />

FIGURE VI.14<br />

. e 10‰2 ‰<br />

rect, other calculation methods<br />

are recommended (Annex F of<br />

EN 1999-1-3). It shall be checked<br />

that the maximum design stress<br />

The fatigue strength is given as<br />

SN curves for the different<br />

details. All detail categories given<br />

<strong>in</strong> EN 1999-1-3 have their own<br />

SN curve. A typical SN curve is<br />

shown on the Figure VI.14.<br />

104 105 106 107 108 109 N<br />

1<br />

m 2<br />

5 . 10 e<br />

N D<br />

a. Fatigue strength curve b. Reference fatigue strength c. Constant amplitude fatigue limit d. Cut-off limit<br />

N L<br />

c<br />

1)<br />

d<br />

range don’t result <strong>in</strong> a tensile<br />

stress exceed<strong>in</strong>g the design stress<br />

<strong>in</strong> ultimate limit state.

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