Surface mechanical attrition treatment (SMAT) methods and systems for modifying nanostructures
US-9809893-B2 · Nov 7, 2017 · US
US10253383B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10253383-B2 |
| Application number | US-201414411102-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 1, 2014 |
| Priority date | Aug 2, 2013 |
| Publication date | Apr 9, 2019 |
| Grant date | Apr 9, 2019 |
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The present invention is about the design and manufacturing method of constructing nano-structured lattices. The design of the four periodic two-dimensional lattices (hexagonal, triangulated, square and Kagome) is described; and the process of making nano-structured lattices is outlined in the present invention.
Opening claim text (preview).
What is claimed is: 1. A nano-structured lattice generated by surface mechanical attrition treatment (SMAT), comprising: a plurality of bar members having end portions; and one or more holes embedded inside the nano-structured lattice, wherein the lattice is two-dimensional; wherein one or more of the bar members comprise one or more nodes for connecting one or more other bar members; and wherein one or more of the bar members are partly treated at each of the end portions around the one or more nodes by the SMAT. 2. The lattice of claim 1 , wherein a grain size at a surface of the one or more SMAT treated bar members has been reduced to form at least one nano-structured layer with grain size in nanometer after being treated by the SMAT. 3. The lattice of claim 1 , wherein the lattice is a square lattice comprising the one or more holes in a square shape, and wherein the one or more holes comprises at least two holes being periodically located along two principal axes of planar space. 4. The lattice of claim 3 , one of the two principal axes defining a horizontal axis, wherein the one or more SMAT treated bar members are horizontal bar members for being subjected to an applied loading along the horizontal axis of the square lattice. 5. The lattice of claim 3 , wherein the one or more SMAT treated bar members are partly treated at their end portion within a circle around the one or more nodes. 6. The lattice of claim 5 , wherein the circle has a radius (R) calculated by: R =(1−1/ k ) l/ 2 where k is SMAT duration in minutes, and l is length of each bar member in millimeters. 7. The lattice of claim 1 , wherein the one or more SMAT treated bar members are treated by the SMAT based on being subjected to a maximum axial stress. 8. The lattice of claim 7 , wherein the maximum axial stress is uniaxial.
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