Page 94 - Biaxial Multiaxial Fatigue and Fracture
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Micro-Cmck Growth Behavior in  Weldments of a Nickel-Base Superalloy Under ...   79



                           5.0   0  ‘41        I             I
                                                     BM
                         -                           A b0.64
                                                     + b-0.50(barf’) -
                                                       +-0.50
                         &?                          rn k-1.00
                         -1  .o
                         a-
                         4 0.5
                      E         WAX       WCF
                      X  t
                      .- i      0 b-0.50   0 k-0.50
                                             @=-l.m
                                A +-0.64
                                0 +-1.00
                      r”   0.11  ‘ g o * 1    1 03          1 o4   I
                                               I
                                                             I
                                102
                               Number of  cycles to failure  Nf
                 Fig. 21. Relationship between maximum principal strain range and failure cycle.
          strain were good parameters for evaluating the crack growth rate, because of the reduction in
          stress  intensity  around  the  crack  tip  due  to  the  effect  of  the  X-like  crack  shape  and  the
          minimum principal strain parallel to the crack, as mentioned above.
            Fatigue strength reduction in a weldment is generally evaluated based on the failure life of
          standard specimens. In  the case of a weldment of Hastelloy-X, fatigue life reduction can be
          explained  by  the  grain  boundary  cracks  induced  by  oxidation  in  the  early  stage  of  life.
          Therefore the fracture mechanics approach is suitable for rationalizing the evaluation of fatigue
          life reduction. The principal stress and strain are appropriate parameters for taking into account
          the stress multiaxiality because the crack growth dominates the fatigue life in both base metal
          and weldment.


          SUMMARY
          We investigated crack growth behaviors in weldments of Hastelloy-X under biaxial low-cycle
          fatigue in order to improve the life assessment techniques for high-temperature components.
          From the results, the following conclusions were, obtained.
          (1) The reduction in the fatigue life of a welded specimen is about 112 and the fatigue strength
            reduction factor is about  1.4. Failure lives in the torsional fatigue tests were about twice
            those in the uniaxial test.
          (2) In low-cycle fatigue tests of welded specimens, 0.5-1.0 mm  long cracks were observed in
            the early stages of life. These cracks initiated at grain boundaries and the oxidation of the
             grain boundary affected the cracking.
          (3) In torsional fatigue tests, the crack growth rate in the early stage of life was smaller than in
            uniaxial tests. This is because of the reduction in stiffness around the crack due to the effect
            of the X-like crack shape and the minimum principal strain being parallel to the crack.
          (4) Crack-growth rates in  weldments were  almost the  same as in base metal so fatigue life
            reduction is considered to be due to the initiated crack lengths. The cyclic J-integral range
            based on principal stress and strain is a suitable parameter for evaluating crack growth rates
             in biaxial stress states.
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