Analysis of the compression behaviour of different composite lattice designs

Author:

Umer R12,Barsoum Z3,Jishi HZ1,Ushijima K4,Cantwell WJ1

Affiliation:

1. Department of Aerospace Engineering, Khalifa University of Science and Technology, United Arab Emirates

2. Centre for Future Materials, University of Southern Queensland, Australia

3. Department of Aeronautical and Vehicle Engineering, KTH Royal Institute of Technology, Sweden

4. Department of Mechanical Engineering, Tokyo University of Science, Japan

Abstract

Four all-composite lattice designs were produced using a lost-mould procedure that involved inserting carbon fibre tows through holes in a core. Following resin infusion and curing, samples were heated to melt the core, leaving well-defined lattice structures based on what are termed BCC, BCCz, FCC and F2BCC designs. Analytical and numerical models for predicting the mechanical properties of the four designs are presented and these results are compared with the experimental data from the quasi-static compression tests. Compression tests on the four lattice structures indicated that the F2BCC lattice offered the highest compression strength, although when normalized by relative density, the BCCz lattice structure out-performed other structures. Similarly, the specific compression strengths were found to be superior to those of more traditional core materials. A number of failure mechanisms were also highlighted, including strut buckling, fracture at the strut-skin joints and debonding of reinforcing members at the central nodes. Finally, it is believed that the properties of these lattices can be further increased using higher fibre volume fractions.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

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