4.6 Article

Compressive Mechanics and Hyperelasticity of Ni-Ti Lattice Structures Fabricated by Selective Laser Melting

Journal

CRYSTALS
Volume 12, Issue 3, Pages -

Publisher

MDPI
DOI: 10.3390/cryst12030408

Keywords

selective laser melting; lattice structure; triply periodic minimal surface; mechanical properties; hyperelasticity

Funding

  1. National Natural Science Foundation of China [52105396]
  2. China Postdoctoral Science Foundation [2020M6824]
  3. Natural Science Foundation of Hubei Province [2021CFB003]
  4. Fundamental Research Funds for the Central Universities [2021IVA053, 2021III027JC]

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Additively manufactured Ni-Ti Gyroid-type TPMS lattice structures exhibit excellent manufacturability and mechanical properties for potential applications in bone implantation. Hyperelastic cycle testing indicates that the properties of the lattice structures gradually stabilize with increasing numbers of cycles, and the residual strain is positively correlated with the maximum strain.
Additively manufactured Ni-Ti lattice structures have controllable bio/mechanical properties, as well as excellent large deformation and damping properties similar to those of natural bone. They have broad application prospects in the field of bone implantation. Triply Periodic Minimal Surface (TPMS) structures are believed to be the most potential and ideal bionic bone structures. In this work, Ni-Ti Gyroid-type TPMS lattice structures were fabricated by selective laser melting (SLM) and their manufacturing fidelity and compression properties were evaluated. By changing the maximum strain value, the hyperelastic recovery performance under cyclic stress was investigated. The results showed that the Ni-Ti Gyroid lattice structures fabricated by SLM had excellent manufacturability (relative density can reach 98.93%) and mechanical properties (elastic modulus is about 130.8 MPa, ultimate strength is about 2.7 MPa). The hyperelastic cycle testing showed that the elastic modulus, yield strength and ultimate strength of the lattice structures tended to stablilize gradually with increasing numbers of cycles. The residual strain increased with the number of cycles, and as the maximum strain increased from 4% to 8%, the residual strain also increased from 1% to 4%.

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