Abstract
Aluminum alloy microlattices have been increasingly used in automotive, aerospace, packaging, defense, machinery, and construction industries due to their superior physical and mechanical properties such as high specific strength and energy absorption capacity. However, design and fabrication of microlattice structures remains a challenge because the structure-property relationship in aluminum microlattices has not been established. To address this issue, AlSi10Mg microlattices with different unit cell structures, number of unit cells, and strut diameters were designed and then fabricated by selective laser melting (SLM). The specific energy, compressive strength, and failure modes of the AlSi10Mg microlattices were examined. Experimental results have shown that the AlSi10Mg microlattices fabricated by SLM exhibited a maximum specific compressive strength of 83.113 MPa·g−1 cm3, which is higher than most metallic and non-metallic microlattices reported in the literature. During compression tests, four different failure modes, including contact region crushing, consecutive diagonal cracks at 45° to the loading direction, elastic/plastic buckling and plastic deformation, and single diagonal crack at 45° to the loading direction, were observed. In addition, the microlattices with different unit cells exhibited different strength-density relationships due to these different failure modes.
Original language | English |
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Article number | 108062 |
Journal | Materials and Design |
Volume | 182 |
DOIs | |
State | Published - Nov 15 2019 |
Externally published | Yes |
Funding
The authors would like to thank Mr. Ben Graham from nTopology for providing us with a license to use nTopology Element, Dr. Andrew Dickerson for providing us with access to the digital microscope, Kenyence VHX-900, and Mr. Shutao Song for the assistance in conducting the compression tests. Authors, H.H. and Y.S., would like to acknowledge the financial supports from the Office of Naval Research under a contract number, N00014-17-1-2559 and the U.S. Army Research Laboratory through cooperative agreement # W911NF-17-2-0172 . Any opinions, findings, and conclusions expressed in this paper are those of the authors and do not necessarily reflect the views of the Office of Naval Research or the U.S. Army Research Laboratory or the U.S. Government. The U.S. Government is authorized to reproduce and distribute reprints for Government purposes notwithstanding any copyright notation herein. Use of scanning electron microscope was made possible through the Materials Characterization Facility (MCF), administered by Advanced Materials Processing and Analysis Center (AMPAC) at the University of Central Florida. The authors would like to thank Mr. Ben Graham from nTopology for providing us with a license to use nTopology Element, Dr. Andrew Dickerson for providing us with access to the digital microscope, Kenyence VHX-900, and Mr. Shutao Song for the assistance in conducting the compression tests. Authors, H.H. and Y.S. would like to acknowledge the financial supports from the Office of Naval Research under a contract number, N00014-17-1-2559 and the U.S. Army Research Laboratory through cooperative agreement #W911NF-17-2-0172. Any opinions, findings, and conclusions expressed in this paper are those of the authors and do not necessarily reflect the views of the Office of Naval Research or the U.S. Army Research Laboratory or the U.S. Government. The U.S. Government is authorized to reproduce and distribute reprints for Government purposes notwithstanding any copyright notation herein. Use of scanning electron microscope was made possible through the Materials Characterization Facility (MCF), administered by Advanced Materials Processing and Analysis Center (AMPAC) at the University of Central Florida.
Funders | Funder number |
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Office of Naval Research | N00014-17-1-2559 |
Army Research Laboratory | W911NF-17-2-0172 |
University of Central Florida |
Keywords
- Additive manufacturing
- Aluminum alloy
- Compressive behavior
- Microlattice
- Selective laser melting