aluminium in commercial vehicles - European Aluminium Association
aluminium in commercial vehicles - European Aluminium Association
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.