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Micro-Cmck Growth Behavior in  Weldmenis of a Nickel-Base Superalloy Under ...   61


          specimens were about half those of base metal specimens regardless of the principal strain ratio
          and strain range. The broken line in the figure was determined by moving the solid line in the
          vertical direction  to  coincide with the uniaxial data of  welded specimens. The exact fatigue
          strength reduction factor was about 1.4.
            Figure 5 shows the Micro-Vickers hardness distribution around the weld line. Both base and
          weld metal had hardened after tests, but the difference in hardness of base and weld metal was
          small. This suggests that no strain concentration is produced around the boundary between base
          and weld metal. Figure 6 shows the von  Mises’ equivalent stress-strain relationship  of  base
          metal and weldment. There was not a distinct difference between base metal and weldment so
          the stress-strain relation of both materials could be considered as the same.

                        -


                        8      700°C                    Base metal(BM)
                        v                                  @=-OSO(bar?’  -
                         U    -                          0 4 =-OS0
                         a
                       4                                 A 4 =-0.64
                                                           4 =-1.00
                        E
                        a 1.0:
                        m a 1.0:
                        c
                        m
                        c                  .‘\*\ ..
                        E
                                                              --
                                                                4
                                                          0
                           0.5-
                        .-  0.5-                     .----
                        .-
                              Welded specimen
                        E  E   -Welded  specimen               111.4  -
                                                                     -
                                                               111.4
                                                 welded(WCF)
                                            Circurn.
                              Axially welded(WAX)
                        .gj   Axially  welded(WAX)   Circurn. welded(WCF)
                        .gj
                                 0           @  @=-0.50
                                   4=-0.50
                                 0 4=-0.50
                                               @=-0.50
                                             @
                                  Number of cycles to failure  Nf
                     Fig. 4. Relationship between Mises’ strain range and failure cycle.








                                          Position (mm)

                     Fig. 5. Micro Vickers hardness of welded specimen after the tests.
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