Dressing with contracting layer for linear tissue sites
Systems, apparatuses, and methods for closing an opening through a surface of a tissue site are described. The system includes a sealing member adapted to cover the opening to form a sealed space and a negative-pressure source adapted to be fluidly coupled to the sealed space to provide negative pressure to the sealed space. The system also includes a contracting layer adapted to be positioned adjacent the opening and formed from a material having a firmness factor and a plurality of holes extending through the contracting layer to form a void space. The holes have a perforation shape factor and a strut angle causing the plurality of holes to collapse in a direction substantially perpendicular to the opening. The contracting layer generates a closing force substantially parallel to the surface of the tissue site to close the opening in response to application of the negative pressure.
1. A system for closing an opening through a surface of a tissue site, the system comprising:
a sealing member configured to cover the opening to form a sealed space;
a negative-pressure source configured to be fluidly coupled to the sealed space to provide negative pressure to the sealed space;
a protective layer configured to be positioned over the opening; and
a contracting layer configured to be positioned over the opening and between the protective layer and the sealing member, the contracting layer formed from a material having a plurality of holes extending through the contracting layer to form a void space, the holes having a perforation shape factor and a strut angle configured to cause the plurality of holes to collapse in a direction substantially perpendicular to the opening,
wherein the contracting layer is configured to generate a closing force substantially parallel to the surface of the tissue site to close the opening in response to application of the negative pressure.
2. The system of claim 1 , wherein the plurality of holes are formed in two or more parallel rows.
3. The system of claim 1 , wherein the strut angle is an angle between a line connecting centers of holes in adjacent rows and an orientation line perpendicular to a direction of the closing force, and the strut angle is about 90 degrees.
4. The system of claim 1 , wherein the strut angle is an angle between a line connecting centers of holes in adjacent rows and an orientation line perpendicular to a direction of the closing force, and the strut angle is less than about 90 degrees.
5. The system of claim 1 , wherein the perforation shape factor of a hole of the plurality of holes is a ratio of a first line segment to a second line segment, the first line segment extending from a center of the hole to a perimeter of the hole in a direction perpendicular to a direction of the closing force and the second line segment extending from a center of the hole to a perimeter of the hole in a direction parallel to the direction of the closing force, and wherein the perforation shape factor of the hole is less than about 1.
6. The system of claim 1 , wherein the perforation shape factor of a hole of the plurality of holes is a ratio of a first line segment to a second line segment, the first line segment extending from a center of the hole to a perimeter of the hole in a direction perpendicular to a direction of the closing force and the second line segment extending from a center of the hole to a perimeter of the hole in a direction parallel to the direction of the closing force, and wherein the perforation shape factor of the hole is more than about 1.
7. The system of claim 1 , wherein the material is a foam material having a firmness factor, the firmness factor is a ratio of density of the foam material in a compressed state to a density of the foam material in an uncompressed state, and the firmness factor is about 5.
8. The system of claim 1 , wherein the material is a foam material having a firmness factor, the firmness factor is a ratio of density of the foam material in a compressed state to a density of the foam material in an uncompressed state, and the firmness factor is about 3.
9. The system of claim 1 , wherein the protective layer is configured to be positioned between the contracting layer and at least a portion of the surface of the tissue site surrounding the opening.
10. An apparatus for closing an opening through a surface of a tissue site, the apparatus comprising:
a contracting layer configured to be positioned over the opening and formed from a material having a plurality of holes extending through the contracting layer to form a void space, the holes having a perforation shape factor and a strut angle configured to cause the plurality of holes to collapse in a direction substantially perpendicular to the opening,
wherein the contracting layer is configured to generate a closing force substantially parallel to the surface of the tissue site to close the opening in response to application of a negative pressure.
11. The apparatus of claim 10 , wherein the plurality of holes are formed in two or more parallel rows.
12. The apparatus of claim 10 , wherein the strut angle is an angle between a line connecting centers of holes in adjacent rows and an orientation line perpendicular to a direction of the closing force, and the strut angle is about 90 degrees.
13. The apparatus of claim 10 , wherein the strut angle is an angle between a line connecting centers of holes in adjacent rows and an orientation line perpendicular to a direction of the closing force, and the strut angle is less than about 90 degrees.
14. The apparatus of claim 10 , wherein the perforation shape factor of a hole of the plurality of holes is a ratio of a first line segment to a second line segment, the first line segment extending from a center of the hole to a perimeter of the hole in a direction perpendicular to a direction of the closing force and the second line segment extending from a center of the hole to a perimeter of the hole in a direction parallel to the direction of the closing force, and wherein the perforation shape factor of the hole is less than about 1.
15. The apparatus of claim 10 , wherein the perforation shape factor of a hole of the plurality of holes is a ratio of a first line segment to a second line segment, the first line segment extending from a center of the hole to a perimeter of the hole in a direction perpendicular to a direction of the closing force and the second line segment extending from a center of the hole to a perimeter of the hole in a direction parallel to the direction of the closing force, and wherein the perforation shape factor of the hole is more than about 1.
16. The apparatus of claim 10 , wherein the material is a foam material having a firmness factor, wherein the firmness factor is a ratio of density of the foam material in a compressed state to a density of the foam material in an uncompressed state, and the firmness factor is about 5.
17. The apparatus of claim 10 , wherein the material is a foam material having a firmness factor, wherein the firmness factor is a ratio of density of the foam material in a compressed state to a density of the foam material in an uncompressed state, and the firmness factor is about 3.
18. A method for closing an opening through a surface of a tissue site, the method comprising:
positioning a contracting layer over the opening, the contracting layer formed from a material having a plurality of holes extending through the contracting layer to form a void space, the plurality of holes having a perforation shape factor and a strut angle;
applying negative pressure to the contracting layer to cause the plurality of holes to collapse in a direction substantially perpendicular to the opening in response to at least one of the perforation shape factor and the strut angle; and
collapsing the contracting layer substantially parallel to the surface of the tissue site to close the opening.
19. The method of claim 18 , further comprising:
positioning a protective layer over the opening; and
positioning a sealing member over the contracting layer to form a sealed space.
20. The method of claim 19 , wherein the contracting layer is adjacent the protective layer.
21. The method of claim 18 , wherein collapsing the contracting layer comprises drawing edges of the contracting layer toward a center of the contracting layer in response to the collapse of the holes of the contracting layer.