Conformable medical dressing with self supporting substrate
US-2016038345-A1 · Feb 11, 2016 · US
US12408939B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12408939-B2 |
| Application number | US-202016923651-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 8, 2020 |
| Priority date | May 9, 2014 |
| Publication date | Sep 9, 2025 |
| Grant date | Sep 9, 2025 |
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Official abstract text for this publication.
A method and apparatus for disrupting material at a tissue site is described. A contact layer may be selected for use on the tissue site and positioned adjacent to the tissue site. The contact layer may include walls defining a plurality of through-holes. A sealing member may be positioned over the contact layer and sealed to tissue surrounding the tissue site to form a sealed space enclosing the contact layer. A negative-pressure source may be fluidly coupled to the sealed space. The negative-pressure source may supply negative pressure to the sealed space and the contact layer to draw tissue into the through-holes to form nodules. The negative pressure may be vented from the sealed space to release the nodules.
Opening claim text (preview).
What is claimed is: 1. A system for debriding a tissue site, comprising: a cover adapted to form a sealed space over the tissue site for receiving a negative pressure from a negative-pressure source; and a tissue interface having a manifold and a debridement tool, the manifold and the debridement tool being integral components of the tissue interface; the manifold adapted to deliver negative pressure to the tissue site; the debridement tool adapted to be positioned between the manifold and the tissue site, the debridement tool comprising a felted foam; a plurality of holes extending through the debridement tool, the plurality of holes being separated from each other by walls, the walls having transverse surfaces extending perpendicular to a surface of the debridement tool that form cutting edges with the surface of the debridement tool, and wherein the plurality of holes have a perforation shape factor that allows the plurality of holes to collapse from a relaxed position to a contracted position in response to an application of negative pressure to the sealed space and to return from the contracted position to the relaxed position in response to a removal of negative pressure from the sealed space; and the plurality of holes being adapted to generate macro-pressure points in the tissue site in the contracted position and the cutting edges being adapted to disrupt the macro-pressure points in 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 the plurality of holes are 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 adapted to collapse the plurality of holes from the relaxed position to the contracted position. 4. The system of claim 3 , wherein the strut angle is about 90 degrees. 5. The system of claim 3 , wherein the strut angle is less than about 90 degrees. 6. The system of claim 1 , wherein: the plurality of holes are adapted to have the perforation shape factor and a strut angle that allows the plurality of holes to collapse from the relaxed position to the contracted position; and the plurality of holes are adapted to collapse from the relaxed position to the contracted position generally perpendicular to a line of symmetry of the debridement tool. 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 the plurality of holes have an average effective diameter of about 5 mm. 9. The system of claim 1 , wherein 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 hole 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 hole of the plurality of holes is hexagonal. 15. The system of claim 1 , wherein a shape of each hole of the plurality of holes is elliptical. 16. The system of claim 1 , wherein a shape of each hole of the plurality of holes is circular. 17. The system of claim 1 , wherein a shape of each hole of the plurality of holes is triangular.
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Suction control thereof · CPC title
with liquid supply means · CPC title
Constructional details of the pressure distribution manifold · CPC title
with a cutting strip, band or chain, e.g. like a chainsaw · CPC title
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