Surgical instrument assembly
US-2024358391-A1 · Oct 31, 2024 · US
US10143485B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10143485-B2 |
| Application number | US-201514708078-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 8, 2015 |
| Priority date | May 9, 2014 |
| Publication date | Dec 4, 2018 |
| Grant date | Dec 4, 2018 |
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Systems, methods, and apparatuses for debriding a tissue site are described. The system includes a manifold and a cover adapted to form a sealed space over the tissue site for providing negative pressure. The system also includes a debridement tool positioned between the manifold and the tissue site. The debridement tool having a tissue-facing surface and a plurality of holes separated from each other by walls. The walls have transverse surfaces extending between the tissue-facing surface and an opposite surface that form cutting edges. The holes have a perforation shape factor that allows the holes to collapse from a relaxed position to a contracted position in response to the application and removal of negative pressure from the sealed space. The cutting edges debride the tissue site in response to movement between the relaxed position and the contracted position.
Opening claim text (preview).
What is claimed is: 1. A system for debriding a tissue site, comprising: a manifold adapted to deliver negative pressure to the tissue site; a cover adapted to form a sealed space over the manifold and the tissue site for receiving a negative pressure from a negative-pressure source; a debridement tool adapted to be positioned between the manifold and the tissue site and having a tissue-facing surface and an opposite surface including a plurality of holes extending through the debridement tool from the tissue-facing surface to the opposite surface, wherein each of the plurality of holes is separated from each other by walls, the walls having transverse surfaces extending between the tissue-facing surface and the opposite surface that form cutting edges with the tissue-facing surface, and wherein each of the plurality of holes has a perforation shape factor that allows each of the plurality of holes to collapse from a relaxed position to a contracted position in response to an application and removal of negative pressure from the sealed space; and wherein the cutting edges are adapted to debride the tissue site in response to movement of the debridement tool between the relaxed position and the contracted position. 2. The system of claim 1 , wherein each of the plurality of holes is adapted to collapse from the relaxed position to the contracted position generally perpendicular to a line of symmetry of the debridement tool. 3. The system of claim 1 , wherein the plurality of holes have the perforation shape factor and a strut angle that are adapted to collapse each of the plurality of holes from the relaxed position to the contracted position. 4. The system of claim 1 , wherein: the plurality of holes are adapted to have the perforation shape factor and a strut angle configured to allow each of the plurality of holes to collapse from the relaxed position to the contracted position; and each of the plurality of holes is adapted to collapse from the relaxed position to the contracted position generally perpendicular to a line of symmetry of the debridement tool. 5. The system of claim 3 , wherein the strut angle is about 90 degrees. 6. The system of claim 3 , wherein the strut angle is less than about 90 degrees. 7. The system of claim 1 , further comprising a fluid source adapted to be fluidly coupled to the sealed space to provide fluid to the sealed space. 8. The system of claim 1 , wherein each of the plurality of holes has an average effective diameter of about 5 mm. 9. The system of claim 1 , wherein holes of the plurality of holes are formed in two or more parallel rows. 10. The system of claim 1 , wherein the perforation shape factor of each of the plurality of holes is less than about 1. 11. The system of claim 1 , wherein a thickness of the debridement tool is about 15 mm. 12. The system of claim 1 , wherein a firmness factor of the debridement tool is about 5. 13. The system of claim 1 , wherein a firmness factor of the debridement tool is about 3. 14. The system of claim 1 , wherein a shape of each of the plurality of holes is hexagonal. 15. The system of claim 1 , wherein a shape of each of the plurality of holes is elliptical. 16. The system of claim 1 , wherein a shape of each of the plurality of holes is circular. 17. The system of claim 1 , wherein a shape of each of the plurality of holes is triangular. 18. The system of claim 1 , wherein the debridement tool comprises a compressed foam. 19. The system of claim 1 , wherein the debridement tool comprises a felted foam. 20. The system of claim 1 , wherein the debridement tool comprises a 3D spacer fabric. 21. The system of claim 1 , wherein the debridement tool comprises a thermoplastic elastomer. 22. The system of claim 1 , wherein the debridement tool comprises a thermoplastic polyurethane.
Scrapers · CPC title
Removing layer of skin tissue, e.g. wrinkles, scars or cancerous tissue · CPC title
with a cutting strip, band or chain, e.g. like a chainsaw · CPC title
obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds {(A61L31/041 takes precedence)} · CPC title
possibility of applying pressure · CPC title
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