Ultrasonic Transducer Tissue Selectivity
US-2024090915-A1 · Mar 21, 2024 · US
US11813642B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11813642-B2 |
| Application number | US-201816046982-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 26, 2018 |
| Priority date | Jul 26, 2017 |
| Publication date | Nov 14, 2023 |
| Grant date | Nov 14, 2023 |
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A system includes a first structure, wherein the first structure lacks space inversion symmetry, and wherein the first structure includes a first elastic lattice. The system further includes a second structure, wherein the second structure lacks space inversion symmetry, and wherein the second structure includes a second elastic lattice. Additionally, the system includes the first structure coupled to the second structure such that the first structure and the second structure have a mirror symmetry to each other.
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The invention claimed is: 1. A system comprising: a vibration source; a first structure, wherein the first structure lacks space inversion symmetry, wherein the first structure comprises a first elastic lattice; a second structure, wherein the second structure lacks space inversion symmetry, wherein the second structure comprises a second elastic lattice; wherein the first structure is coupled to the second structure; wherein each of the first elastic lattice and the second elastic lattice have a mirror symmetry to each other; and wherein an interface of the first structure and the second structure is configured to propagate a unidirectional wave from the vibration source. 2. The system of claim 1 , wherein the vibrational source comprises at least one of an engine, a fluid, a gas. 3. The system of claim 1 , wherein the first elastic lattice is configured to generate a plurality of frequency bandgaps, wherein each frequency bandgap of the plurality of frequency bandgaps is obtained around a former Dirac point. 4. The system of claim 3 , wherein the former Dirac point comprises degenerate bands with locally linear dispersion. 5. The system of claim 4 , wherein the degenerate bands with locally linear dispersion occur around a plurality of symmetry points of a hexagonal reciprocal unit cell of the first elastic lattice. 6. The system of claim 5 , wherein each symmetry point of the plurality of symmetry points of the hexagonal reciprocal unit of the first structure comprises K and K′. 7. The system of claim 1 , wherein the second elastic lattice is configured to generate a plurality of second frequency bandgaps, wherein each second frequency bandgap of the plurality of second frequency bandgaps is obtained around a former Dirac point of the second elastic lattice. 8. The system of claim 7 , wherein the former Dirac point comprises degenerate bands with locally linear dispersion of the second elastic lattice. 9. The system of claim 8 , wherein the degenerate bands with locally linear dispersion occur around a plurality of symmetry points of a hexagonal reciprocal unit cell of the second elastic lattice. 10. The system of claim 9 , wherein each symmetry point of the plurality of symmetry points of the hexagonal reciprocal unit of the second elastic lattice comprises K and K′. 11. The system of claim 1 , wherein the first structure is coupled to the second structure comprises: the first structure glued, jointed, or welded to the second structure. 12. The system of claim 1 , wherein the first structure and the second structure are monolithic. 13. The system of claim 1 , wherein the first elastic lattice and the second elastic lattice are acoustically insulating. 14. The system of claim 1 , wherein a lack of space inversion of the first elastic lattice is functionally graded or constant, and wherein a lack of space inversion of the second elastic lattice is functionally graded or constant. 15. The system of claim 1 , wherein a lack of space inversion of the first elastic lattice is functionally graded or constant, or wherein a lack of space inversion of the second elastic lattice is functionally graded or constant. 16. The system of claim 1 , wherein the first structure comprises at least one aluminum, iron, titanium, copper, steel, brass, glass, polymers, glass fibers, carbon fibers, poly paraphenylene terephthalamide, plastics, ceramics, zinc, chromium, or nickel, and wherein the second structure comprises at least one of aluminum, iron, titanium, polymers, glass fibers, carbon fibers, poly paraphenylene terephthalamide, plastics, ceramics, zinc, chromium, or nickel. 17. The system of claim 1 , wherein the first structure has a thickness, wherein the thickness is approximately 1/10th or lower of a characteristic in-plane dimension. 18. The system of claim 17 , wherein the characteristic in-plane dimension comprises a length or a width. 19. The system of claim 1 , wherein the first structure further comprises a top layer and a bottom layer, wherein the top layer is connected to a top surface of the first structure, and the bottom layer is connected to a bottom surface of the first structure. 20. The system of claim 1 , wherein the second structure further comprises a top layer and a bottom layer, wherein the top layer is connected to a top surface of the second structure, and the bottom layer is connected to a bottom surface of the second structure. 21. The system of claim 1 , wherein the first elastic lattice comprises a geometry, wherein the geometry is configured to generate hexagonal reciprocal unit cell. 22. The system of claim 1 , wherein the frequency second elastic comprises a geometry, wherein the geometry is configured to generate hexagonal reciprocal unit cell.
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