Apparatus, system, and method for repairing composite sandwich panels

Patent metadata

Field	Value
Publication number	US-12064929-B2
Application number	US-202217718020-A
Country	US
Kind code	B2
Filing date	Apr 11, 2022
Priority date	Jun 2, 2021
Publication date	Aug 20, 2024
Grant date	Aug 20, 2024

Abstract

Disclosed herein are a repair apparatus, system, and method for a composite sandwich structure. The repair is suited for reinforcing a sandwich panel having a first sheet and a second sheet opposite the first sheet. A core is interposed between and coupled to the first sheet and the second sheet. The repair uses a potting compound packed into an abnormality of the core and located on the outer surface of the first sheet. A patch is coupled to the outer surface of the first sheet over the abnormality of the core and cured. The cured potting compound is interposed between and bonded to the patch and the abnormality of the core and bonded to the patch and the outer surface of the first sheet to form a structural reinforcement.

First claim

What is claimed is:

1. A method of installing a structural reinforcement on a sandwich structure, the method comprising:
removing a portion of a first sheet and a core of the sandwich structure to form a cavity in the first sheet and the core of the sandwich structure;
filling the cavity in the sandwich structure with an uncured potting compound such that at least a portion of the uncured potting compound extends onto an outer surface of the first sheet;
applying the uncured potting compound on a surface of a patch;
covering the cavity in the core and the outer surface of the first sheet with the patch, wherein:
the uncured potting compound extends between an inner surface of a second sheet of the sandwich structure and the patch to repair an abnormality in the core of the sandwich structure; and
the uncured potting compound extends between the outer surface of the first sheet of the sandwich structure and the patch to adhere the patch to the first sheet; and

curing the uncured potting compound.

2. The method of claim 1 , wherein removing a portion of the first sheet and the core to form the cavity further comprises abrading the outer surface of the first sheet.

3. The method of claim 1 , wherein the method further comprises, prior to filling the cavity with the uncured potting compound:
removing a coating layer on the first sheet surrounding the cavity;
penetrating the core under the first sheet to create the cavity extending to the second sheet; and
removing a loose fiber from the coating layer on the outer surface of the first sheet.

4. The method of claim 1 , wherein the method further comprises, prior to filling the cavity with the uncured potting compound:
removing debris from the cavity in the core; and
heating the core to remove moisture.

5. The method of claim 1 , wherein the method further comprises, prior to applying the uncured potting compound onto the surface of the patch, penetrating the patch to create a relief hole extending between a second surface of the patch and the surface that the uncured potting compound is to be applied to the patch.

6. The method of claim 1 , wherein filling the cavity with the uncured potting compound further comprises packing the uncured potting compound into the cavity until the uncured potting compound abuts an inner surface of the first sheet, such that when the uncured potting compound is cured, the inner surface of the second sheet bonds to the inner surface of the first sheet.

7. The method of claim 1 , wherein, the method further comprises, after covering the cavity with the patch and prior to curing the uncured potting compound:
removing excess uncured potting compound from the outer surface of the first sheet; and
removing excess uncured potting compound adjacent to a relief hole from a second surface of the patch.

8. The method of claim 1 , wherein the method further comprises, after covering the cavity with the patch and prior to curing the uncured potting compound:
applying a vacuum bag and a heat blanket over the patch;
applying heat with the heat blanket and reducing pressure locally within the vacuum bag; and
curing the uncured potting compound to form a thermoset bond between the patch and the outer surface of the first sheet.

9. The method of claim 1 , wherein the method further comprises, prior to covering the cavity with the patch:
packing loose fibers into the uncured potting compound; and
curing the uncured potting compound with the loose fibers packed in the uncured potting compound.

10. The method of claim 1 , further comprising installing a bushing within the cavity and the uncured potting compound, wherein the bushing extends through a relief hole in the patch.

11. The method of claim 1 , further comprising heating the patch to mold the structural reinforcement, wherein:
the patch comprises an area and a contour;
a first ply is pre-arranged in a predefined orientation relative to a second ply in the patch; and
heating the patch at least partially bonds the first ply to the second ply in the patch and changes the contour of the structural reinforcement.

12. The method of claim 1 , wherein curing the uncured potting compound forms a cured sandwich structure comprising:
the first sheet;
the second sheet, which is opposite the first sheet;
the core, which is interposed between and coupled to the first sheet and the second sheet;
the cavity, which is filled with cured potting compound;
a structural reinforcement coupled to the outer surface of the first sheet over and in the cavity, the structural reinforcement comprising:
the patch, which comprises a ply; and
the cured potting compound packed into the cavity and further located on the outer surface of the first sheet; wherein:
the cured potting compound is interposed between and bonded to the patch and the cavity; and
the cured potting compound is interposed between and bonded to the patch and the outer surface of the first sheet.

13. The method of claim 12 , further comprising disposing in the patch a relief hole extending through a thickness of the patch, wherein a portion of the cured potting compound is located within the relief hole.

14. The method of claim 12 , further comprising defining within the core a honeycomb structure such that the honeycomb structure is adjacent to the cavity, wherein:
the honeycomb structure provides the first sheet and the second sheet a design bending strength;
the cured potting compound in the cavity provides a repair bending strength; and
the repair bending strength is equal to or greater than the design bending strength.

15. The method of claim 12 , further comprising disposing a bushing within the sandwich structure, wherein:
the core is a honeycomb structure that surrounds the cured potting compound; and
the cured potting compound surrounds the bushing.

16. The method of claim 12 , wherein:
the sandwich structure is an aircraft comprising an external wetted surface; and
the outer surface of the first sheet and the patch of the structural reinforcement define the external wetted surface of the aircraft.

17. The method of claim 12 , wherein the core is made of a foam material and the cured potting compound extends through a partial thickness of the core.

18. The method of claim 12 , wherein the first sheet further comprises:
an inner surface opposite the outer surface; and
a peripheral edge through a thickness of the first sheet that extends between the outer surface and the inner surface of the first sheet;
the second sheet further comprises an inner surface;
the patch comprises a first surface opposite a second surface; and
the cured potting compound is bonded to a portion of the inner surface of the first sheet, to the peripheral edge of the first sheet, to the inner surface of the second sheet, to an entirety of the first surface of the patch, and to a portion of the second surface of the patch.

19. The method of claim 18 , further comprising directly interposing an adhesive between the second sheet and the cured potting compound in the cavity.

20. The method of claim 12 , wherein the patch comprises:
a first ply having fibers embedded in a matrix to provide a strength to the first ply, the first ply defining a surface of the patch that is bonded to the cured potting compound; and
a second ply having fibers embedded in a matrix to provide a strength to the second ply, wherein the first ply is oriented relative to the second ply to provide a predetermined reinforcement strength to the p

Assignees

• Boeing Co

Inventors

• Staal Remmelt Andrew
• Register Justin H
• Fidgeon Ernie
• Edwards Glory C
• Smith Gregory J

Classifications

• B29C73/10

  using patches sealing on the surface of the article (B29C73/14 takes precedence) · CPC title

• B29C73/26 Primary

  for mechanical pretreatment · CPC title

• B29C2073/264

  for cutting out or grooving the area to be repaired · CPC title

• B29C73/02 Primary

  using liquid or paste-like material (B29C73/16 takes precedence) · CPC title

• B29C73/34

  for local heating · CPC title