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24                           G. SAVAIDIS ET AL

            spot stress approach, see e.g. Bovet-Griffon et al. [5] and Fayard et al. [6]. Further experience
            gathered  on  thin-walled  plane  structures  of  commercial  vehicle  components  under
            proportional  constant amplitude normal stresses [7] revealed that fatigue analysis based on hot
            spot stresses is capable of handling such components.
              The local  stress approach  to fatigue of  welded joints represents  an  alternative  to the hot
            spot stress approach. Its  main  advantage can be seen  in  the  existence of  an  experimentally
            verified  universal  constant  amplitude local  stress-life  curve  for  steel  welds.  However,  the
            determination of local stresses causes a clearly increasing numerical effort.
              This  paper  deals  with  the  critical  plane  approach  in  connection  with  numerically
            determined  hot  spot  stresses;  particularly,  its  application  to  nonproportional  variable
            amplitude loading is shown and discussed. In the latter part of the paper the application  of the
            local  stress approach is shown. A comparison of fatigue lives gained from hot spot stresses,
            local stresses and experimental investigation, respectively, will close the paper.


            COMPONENT AND LOAD CONFIGURATION
            The component under investigation is a thin-walled tube joined at both ends to forged arms by
            fillet welding. This component serves to stabilise the driver’s cab of trucks. The mechanical
            behaviour  and the fatigue life of the component shown in Fig. 1 are calculated and compared
            with corresponding test results.














            Fig.  1. Component under investigation


              Figure 2 shows the test  rig with  two actuators at the top left-hand  side of the component
            capable for introducing lateral  forces and forces resulting  from suspension. Figure 3 shows
            the normalised force-time sequences Fy(t) and F,(t) that have been measured using a prototype
            component during driving on a test track. The test track driving program includes quasi-static
            manoeuvres like cornering, braking during cornering and braking at straight-driving  as well as
            straight-driving over rough  road  segments like potholes,  washboards, belgian  block, country
            roads  and  rough  highways.  The  corresponding  spectra  of  the  normalised  forces  versus
            cumulative frequency of occurrence evaluated  in accordance with the level crossing counting
            method provide  approximately straight-line  shaped distributions and cumulative number  of
            cycles of approximately 3500 for Fy(t) and 2300 for F,(t) for one block. The running time for
            the experimental simulation of one block on the test rig amounts to approximately 28 minutes.
              These  load  components  predominantly  cause  bending  (Mx, M,)  and torsion  (My) which
            interact nonproportionally.
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