Guanchen Si, Zheng Xiang, Qin Yang, Xianfeng Shen, Jie Chen, Shuke Huang. Effects of Cell Configuration and Micro Defects on Fatigue Properties of NiTi Alloy Lattice Structure Having with Rigidity Prepared by SLM[J]. Laser & Optoelectronics Progress, 2023, 60(21): 2114009

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- Laser & Optoelectronics Progress
- Vol. 60, Issue 21, 2114009 (2023)

Fig. 1. Unit cell and structure models for BCCZ, FCCZ, and FBCCZ

Fig. 2. NiTi alloy powder. (a) Microscopic image; (b) particle size distribution

Fig. 3. NiTi alloy lattice structure
![Material properties and boundary condition used in simulation[24]. (a) Tensile data for SLM NiTi material; (b) boundary conditions](/Images/icon/loading.gif)
Fig. 4. Material properties and boundary condition used in simulation[24]. (a) Tensile data for SLM NiTi material; (b) boundary conditions

Fig. 5. Compression test results of BCCZ, FBCCZ, and FCCZ structures. (a) Stress-strain curves; (b) yield stress and elastic modulus

Fig. 6. Fatigue test results of BCCZ, FBCCZ, and FCCZ structures. (a) Absolute fatigue life curves; (b) normalized fatigue life curves

Fig. 7. Morphologies of three structures after fatigue failure. (a) BCCZ; (b) FCCZ; (c) FBCCZ

Fig. 8. Cracks generated at the pillar nodes after fatigue failure of three structures. (a) BCCZ; (b) FCCZ; (c) FBCCZ

Fig. 9. Pore distribution and pore morphology. (a) BCCZ; (b) FCCZ; (c) FBCCZ

Fig. 10. Statistics of hole defects. (a) Diameter distribution of hole defects; (b) volume fraction of hole defects

Fig. 11. Simulation results of three structures under 30 MPa stress. (a) BCCZ; (b) FCCZ ; (c) FBCCZ

Fig. 12. Simulation results of three structures under 15 MPa stress. (a) BCCZ; (b) FCCZ ; (c) FBCCZ

Fig. 13. SEM of fracture after fatigue failure under low stress. (a) BCCZ; (b) FCCZ; (c) FBCCZ

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