초록 ▼

Systems and methods for providing a structural adhesive film that includes a conductive scrim layer are disclosed. In one embodiment, a method for producing a structural adhesive film includes providing a first resin adhesive layer. The first resin adhesive layer is configured to bind to a first car

Systems and methods for providing a structural adhesive film that includes a conductive scrim layer are disclosed. In one embodiment, a method for producing a structural adhesive film includes providing a first resin adhesive layer. The first resin adhesive layer is configured to bind to a first carbon fiber ply. The method also includes providing a second resin adhesive layer. The second adhesive layer is configured to bind to a second carbon fiber ply. The method also includes providing a conductive scrim that is embedded between the first resin adhesive layer and the second resin adhesive layer. In some embodiments, the conductive scrim is infused with resin adhesive.

대표청구항 ▼

What is claimed is: 1. A method for using conductive scrim embedded structural adhesive films, comprising: providing a stepped recess that penetrates a surface of a repair area to remove a portion of a reinforced component, the reinforced component having an original outer shape; positioning a firs

What is claimed is: 1. A method for using conductive scrim embedded structural adhesive films, comprising: providing a stepped recess that penetrates a surface of a repair area to remove a portion of a reinforced component, the reinforced component having an original outer shape; positioning a first conductive structural adhesive film that includes a first conductive scrim into the stepped recess that penetrates the surface of the repair area and at least partially on a first step of the stepped recess; inserting a first laminate ply into the stepped recess on top of the first conductive structural adhesive film; positioning a second conductive structural adhesive film that includes a second conductive scrim into the stepped recess so that the second conductive scrim is at least partially on a second step of the stepped recess and in contact with the first conductive scrim and the first laminate ply, the first step being further away from the surface of the repair area than the second step; inserting one or more second laminate plies into the stepped recess on top of the second conductive structural adhesive film to fill the repair area; disposing a third conductive structural adhesive film on top of the repair area, wherein the third conductive structural adhesive film includes a third conductive scrim; disposing one or more third laminate plies on top of the third conductive structural adhesive film; and curing the laminate plies disposed inside and on top of the repair area. 2. The method of claim 1, wherein the reinforced component includes at least one conductive layer, and wherein disposing a third conductive structural adhesive film includes establishing electrical contact between the third conductive scrim and a portion of the at least one conductive layer. 3. The method of claim 1, wherein the one or more second laminate plies are configured to restore the carbon fiber reinforced component to at least the original outer shape. 4. The method of claim 1, and wherein reinforced component includes a carbon fiber reinforced component, and wherein each of the first laminate plies, the second laminate plies, and the one or more third laminate plies include carbon fiber laminate plies. 5. The method of claim 1, wherein inserting one or more second laminate plies includes orienting each second laminate ply with the corresponding ply of the reinforced component. 6. The method of claim 1, wherein at least one of the first conductive scrim, the second conductive scrim, or the third conductive scrim includes metallic conductive fibers, the metallic conductive fibers include at least one of copper, aluminum, platinum, or silver fibers. 7. The method of claim 1, wherein providing a stepped recess including providing a stepped recess to a repair area that is located on a vehicle. 8. The method of claim 1, wherein providing a stepped recess including providing a stepped recess to a repair area that is located on an aircraft. 9. The method of claim 1, further comprising producing one or more conductive scrim embedded structural adhesive films, wherein producing each of the conductive scrim embedded structural adhesive films includes: providing a first carbon fiber ply and a second carbon fiber ply that do not include metallic conductive fibers; providing a first resin adhesive layer that binds to the first carbon fiber ply; providing a second resin adhesive layer that binds to the second carbon fiber ply; and providing a resin adhesive infused conductive scrim that is disposed between and bonded to the first resin adhesive layer that binds to the first carbon fiber ply and the second resin adhesive layer that binds to the second carbon fiber ply. 10. The method of claim 1, wherein at least one of the first conductive scrim the second conductive scrim, or the third conductive scrim includes randomly-oriented metallic conductive fibers. 11. A method for using conductive scrim embedded structural adhesive films, comprising: providing a stepped recess that penetrates a surface of a repair area to remove a portion of a reinforced component, the reinforced component having an original outer shape; positioning a first conductive structural adhesive film that includes a first conductive scrim into the stepped recess that penetrates the surface of the repair area and at least partially on a first step of the stepped recess; inserting a first laminate ply into the stepped recess on top of the first conductive structural adhesive film; positioning a second conductive structural adhesive film that includes a second conductive scrim into the stepped recess so that the second conductive scrim is at least partially on a second step of the stepped recess and in contact with the first conductive scrim and the first laminate ply, the first step being further away from the surface of the repair area than the second step; inserting one or more second laminate plies into the stepped recess on top of the second conductive structural adhesive film to fill the repair area; disposing a third conductive structural adhesive film on top of the repair area, wherein the third conductive structural adhesive film includes a third conductive scrim; and disposing one or more third laminate plies on top of the third conductive structural adhesive film. 12. The method of claim 11, wherein the reinforced component includes at least one conductive layer, and wherein disposing a third conductive structural adhesive film includes establishing electrical contact between the third conductive scrim and a portion of the at least one conductive layer. 13. The method of claim 11, and wherein reinforced component includes a carbon fiber reinforced component, and wherein each of the first laminate plies, the second laminate plies, and the one or more third laminate plies include carbon fiber laminate plies. 14. The system of claim 11, wherein inserting one or more second laminate plies includes orienting each second laminate ply with the corresponding ply of the reinforced component. 15. The method of claim 11, wherein at least one of the first conductive scrim, the second conductive scrim, or the third conductive scrim includes metallic conductive fibers. 16. The method of claim 11, wherein providing a stepped recess including providing a stepped recess to a repair area that is located on a vehicle. 17. The method of claim 11, wherein providing a stepped recess including providing a stepped recess to a repair area that is located on an aircraft. 18. The method of claim 11, further comprising producing one or more conductive scrim embedded structural adhesive films, wherein producing each of the conductive scrim embedded structural adhesive films includes: providing a first carbon fiber ply and a second carbon fiber ply that do not include metallic conductive fibers; providing a first resin adhesive layer that binds to the first carbon fiber ply; providing a second resin adhesive layer that binds to the second carbon fiber ply; and providing a resin adhesive infused conductive scrim that is disposed between and bonded to the first resin adhesive layer that binds to the first carbon fiber ply and the second resin adhesive layer that binds to the second carbon fiber ply. 19. The method of claim 11, wherein at least one of the first conductive scrim, the second conductive scrim, and the third conductive scrim includes randomly-oriented metallic conductive fibers. 20. A method for using conductive scrim embedded structural adhesive films, comprising: providing a stepped recess that penetrates a surface of a repair area to remove a portion of a reinforced component, the reinforced component having an original outer shape; positioning a first conductive structural adhesive film that includes a first conductive scrim into the stepped recess that penetrates the surface of the repair area and at least partially on a first step of the stepped recess; inserting a first laminate ply into the stepped recess on top of the first conductive structural adhesive film; positioning a second conductive structural adhesive film that includes a second conductive scrim into the stepped recess so that the second conductive scrim is at least partially on a second step of the stepped recess and in contact with the first conductive scrim and the first laminate ply, the first step being further away from the surface of the repair area than the second step; and inserting one or more second laminate plies into the stepped recess on top of the second conductive structural adhesive film to fill the repair area. 21. The method of claim 20, further comprising positioning one or more third laminate plies under the surface of the repair area and on the stepped recess so that at least one of the one or more third laminate plies contacts the first conductive scrim. 22. The method of claim 20, and wherein reinforced component includes a carbon fiber reinforced component, and wherein each of the first and second laminate plies include carbon fiber laminate plies. 23. The method of claim 20, wherein at least one of the first conductive scrim or the second conductive scrim includes metallic conductive fibers. 24. The method of claim 20, wherein providing a stepped recess including providing a stepped recess to a repair area that is located on a vehicle or an aircraft. 25. The method of claim 20, further comprising producing one or more conductive scrim embedded structural adhesive films, wherein producing each of the conductive scrim embedded structural adhesive films includes: providing a first carbon fiber ply and a second carbon fiber ply that do not include metallic conductive fibers; providing a first resin adhesive layer that binds to the first carbon fiber ply; providing a second resin adhesive layer that binds to the second carbon fiber ply; and providing a resin adhesive infused conductive scrim that is disposed between and bonded to the first resin adhesive layer that binds to the first carbon fiber ply and the second resin adhesive layer that binds to the second carbon fiber ply.