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          8.0 Fatique in welded joints Welding handbook










          8.4 Weld quality
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          Weld quality is very important to the fatigue strength
          of the welded joint. Higher loads demand better            Stop
          weld quality. In EN ISO 5817, there are defined weld
          quality classes, these, however, are not related to the
                                                                                             Direction
          fatigue strength of a welded joint.                                                of welding



                                                                                            Do not stop
                                                                                  Weld here  weld here
            Solidification crack  Concavity
            Undercut          Underfill
                                                               Force
            Lack of penetration  Lack of side      Cold lap
                              wall fusion
                                                           Fig. 8.8: Place starts and stops at the side of the attachment
                                                           longitudinally, not at the end of the weld.
            Hydrogen crack   Overfill  Excess root gap
            Slag                     Lamellar tearing
            Porosity                                       The welding process and the filler material affect the
                                                           fatigue strength at the transition point between the
                                                           weld metal and the parent material. They also affect
          Fig. 8.7: Examples of discontinuities in a welded joint.   the amount of discontinuities in the welded joint.
                                                           The process and the filler material, therefore, should
                                                           be chosen in a way that minimizes these effects.
          Generally, crack-like discontinuities are more severe   Differences in strength between the filler material
          than rounded discontinuities and discontinuities close   and the parent material have no proven effect on the
          to the surface are more severe as well. Solidification   fatigue strength.
          cracks, hydrogen cracks and lack of penetration cannot
          be tolerated in fatigue-loaded structures. Cold laps and
          under cuts should be avoided as well. Small rounded   8.5 Nominal stress method
          pores in the welded joints have a very small influence   This section is a short introduction to dimension
          on the fatigue strength.                         and designing of fatigue in welded joints.

          Design discontinuities like starts and stops should    The nominal stress method is based on categorizing
          be placed on low stressed areas or non-loaded    weld geometries into joint classes. Depending on the
          components. For cases when the above cannot be   standard of use, these joint classes are designated
          achieved, starts and stops should be grinded down.   differently; notch class (NC) for EN 1993-1-9,
                                                           Δσc in EN 13001, etc. FAT is the designation in
                                                           the International Institute of Welding (IIW)
                                                           “Recommendation for fatigue design of welded
                                                           joints and components”. Henceforth, FAT will be
                                                           used to designate joint classes in general. The FAT
                                                           value is defined as the characteristic fatigue strength
                                                           at 2 million cycles. Modifying formula 8.1 gives:


                                                                                  1
                                                                          2 x 10 6  m
                                                            ∆ σ = FAT                     Fomula 8.2
                                                                           N

          50      This handbook contains general suggestions and information without any expressed or implied warranty of any kind. SSAB hereby expressly disclaims
                    all liability of any kind, including any damages, in connection with the use of the information and for their suitability for individual applications.
                   It is the responsibility of the user of this brochure to adapt the recommendations contained therein to the requirements of individual applications.
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