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Materials Science in Additive Manufacturing                            NiTi lattice: Performance optimization



            efficiency,  when the lattice structure collapses and breaks,   corresponding to this point decreased, indicating that a
                    24
            the stress value as the denominator decreases sharply in   smaller load could improve the fatigue life.
            a small strain range, resulting in an inflection point and   The curve bulge observed in the initial stage, as shown
            a rapid rise in the energy absorption efficiency curve. It   in (Figure 5A and B), is attributed to the instability of the
            can be concluded that during compression, the lattice   fatigue  testing machine  at the  initial stage  of  operation.
            structures improve the energy absorption efficiency
            through the deformation of struts.                 Since the load ratio of the fatigue test was set to R = 0.1, the
                                                               minimum value of the load set in the test conditions was too
            3.3. Fatigue performance                           small relative to the working load range of the equipment,
            3.3.1. Strain accumulation                         so the fatigue test machine was unstable during the initial
                                                               operation cycles. The changes in applied load and indenter
            Figure  5A and  B show the accumulative strain-cycle   position during the operation of the machine are plotted in
            curves of the two lattice structures at different stress   (Figure 5C). Between 10 and 100 cycles, the values of the
            levels, respectively. The strains of the two structures   load and indenter position were not stable, and a region of
            gradually increased and accumulated with the increase   fluctuation in the load and indenter position curves was
            of the cycles, and the compression height of the sample   observed, corresponding to the fluctuations in the strain
            was reduced. The strain accumulation curves can be   accumulation curves in (Figure 5A and B).
            divided into three stages: the initial strain increase stage
            (N < 50), the constant strain plateau stage, and the rapid   The accumulative strain per cycle was calculated as
            strain accumulation stage. As shown in (Figure 5A and B),   shown in (Figure  5D). By calculating the cumulative
            between the constant strain plateau stage and the rapid   strain per cycle before the strain mutation point in
            strain accumulation stage, the abrupt strain point, N  can   (Figure 5A and B), we found that the larger the load, the
                                                      c
            be clearly observed in the strain accumulation curves.   higher the cumulative strain per cycle. In addition, the
            As the loading stress increased, the strain value of the   I-WP exhibited a much lower accumulative strain per
            abrupt strain point also increased, but the cycle number   cycle than the BCC in high-cycle fatigue (low-stress level),

                         A                                   B















                         C                                   D


















            Figure 5. Accumulative strain-cycle curves, as well as changes of force and indenter position during fatigue test. (A and B) Accumulative strain-cycle
            curves of body-centered cubic (BCC) (A) and I-graph-wrapped package (B). (C and D) Variation of force and indenter position of the fatigue test machine
            during fatigue tests: BCC1.71 MPa (C), and accumulative strain per cycle (D).


            Volume 3 Issue 2 (2024)                         7                              doi: 10.36922/msam.3380
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