Systems and methods for adhesive-injected patch repair

Patent metadata

Field	Value
Publication number	US-11718050-B2
Application number	US-202117551322-A
Country	US
Kind code	B2
Filing date	Dec 15, 2021
Priority date	Dec 17, 2020
Publication date	Aug 8, 2023
Grant date	Aug 8, 2023

Abstract

In an example, a method is described. The method comprises placing a repair patch over a repair area of a structure, the repair patch comprising a repair-patch hole. The method also comprises sealing the repair patch and repair area with a vacuum bag having a seal ring around a periphery of the vacuum bag. The method also comprises evacuating, via an adhesive injection apparatus attached to the repair-patch hole and the seal ring of the vacuum bag, the repair area and an injection channel of the adhesive injection apparatus. The method also comprises forcing adhesive through the evacuated injection channel and into the evacuated repair area.

First claim

What is claimed is:

1. A method comprising:
placing a repair patch over a repair area of a structure, the repair patch comprising a repair-patch hole;
sealing the repair patch and repair area with a vacuum bag having a seal ring around a periphery of the vacuum bag;
evacuating, via an adhesive injection apparatus attached to the repair-patch hole and the seal ring of the vacuum bag, the repair area and an injection channel of the adhesive injection apparatus; and
forcing adhesive through the evacuated injection channel and into the evacuated repair area.

2. The method of claim 1 , wherein sealing the repair patch and repair area with the vacuum bag comprises engaging the seal ring with the structure by drawing a vacuum through a seal actuation tube of the adhesive injection apparatus that is fluidly coupled to the seal ring.

3. The method of claim 1 , further comprising:
evacuating a transfer channel fluidly coupled to an adhesive reservoir of the adhesive injection apparatus,
wherein forcing the adhesive through the evacuated injection channel and into the evacuated repair area comprises forcing the adhesive through the evacuated transfer channel to the evacuated injection channel and into the evacuated repair area.

4. The method of claim 3 , wherein:
the adhesive injection apparatus comprises (i) a three-way valve fluidly coupled to the transfer channel, the injection channel that is coupled to the repair area, and an evacuation channel that is coupled to a vacuum source and (ii) a seal actuation tube fluidly coupled to the seal ring and the evacuation channel,
evacuating the repair area comprises positioning the three-way valve to establish fluid communication between the evacuation channel and the injection channel,
evacuating the transfer channel comprises positioning the three-way valve to establish fluid communication between the evacuation channel and the transfer channel, and
forcing the adhesive through the evacuated transfer channel to the evacuated injection channel and into the evacuated repair area comprises positioning the three-way valve to establish fluid communication between the evacuated transfer channel and the evacuated injection channel.

5. The method of claim 1 , wherein placing the repair patch over the repair area of the structure comprises placing a patch of pre-cured composite over the repair area of the structure.

6. The method of claim 1 , wherein:
placing the repair patch over the repair area of the structure comprises placing a multi-layer patch over the repair area of the structure, the multi-layer patch having multiple layers separated by a plurality of bondline spacers,
the multiple layers of the multi-layer patch comprise layers of one or more of a sheet metal, a polymer, or a pre-cured composite, and
forcing adhesive through the evacuated injection channel and into the evacuated repair area further comprises forcing adhesive into the multi-layer patch between the multiple layers.

7. The method of claim 6 , further comprising:
before sealing the repair patch and repair area with the vacuum bag, placing breather and release plies over the repair patch.

8. The method of claim 1 , wherein forcing the adhesive through the evacuated injection channel and into the evacuated repair area comprises forcing a de-aerated adhesive through the evacuated injection channel and into the evacuated repair area.

9. The method of claim 1 , wherein placing the repair patch over the repair area of the structure comprises placing the repair patch over a plurality of bondline spacers positioned between the repair patch and the structure and configured to maintain a desired gap between the repair patch and the structure.

10. The method of claim 1 , wherein the vacuum bag comprises a float valve configured to prevent the adhesive from flowing into the seal ring.

11. The method of claim 1 , further comprising:
detecting that the adhesive fills the repair area via a fill sensor disposed proximate to the seal ring.

12. The method of claim 11 , wherein detecting that the adhesive fills the repair area via the fill sensor disposed proximate to the seal ring comprises detecting that the adhesive fills the repair area via a fill sensor selected from the group consisting of a radio frequency identification (RFID) tag configured to modulate frequency response based on the adhesive contacting the RFID tag, a piezo electric sensor configured to change a response as the adhesive moves toward the piezo electric sensor and based on the adhesive contacting the piezo electric sensor, a capacitive sensor configured to respond to adjacent adhesive, a conductive sensor configured to respond to adhesive wetting and resulting conductivity changes by contact, and a resistive sensor configured to respond to adhesive wetting and resulting resistance changes by contact.

13. The method of claim 1 , further comprising:
before evacuating the repair area and the injection channel, attaching the adhesive injection apparatus to the repair-patch hole and sealing the adhesive injection apparatus against the vacuum bag with vacuum seal tape.

14. The method of claim 1 , wherein sealing the repair patch and repair area with the vacuum bag comprises sealing the repair patch and the repair area with a vacuum bag having embedded in a plurality of heating elements.

15. The method of claim 14 , further comprising:
after forcing the adhesive through the evacuated injection channel and into the evacuated repair area, heating the adhesive using the plurality of heating elements, wherein heating the adhesive at least partially cures the adhesive and repairs the repair area.

16. The method of claim 1 , wherein the forcing of adhesive through the injection channel includes breaking a frangible seal.

17. An adhesive injection apparatus comprising:
a transfer channel configured to be fluidly coupled to an adhesive reservoir;
an injection channel configured to be fluidly coupled to a repair area;
an evacuation channel configured to be fluidly coupled to a vacuum source;
a seal actuation tube configured to be fluidly coupled to the evacuation channel and a seal ring around a periphery of a vacuum bag, wherein the vacuum bag is used to seal a repair patch and the repair area; and
a three-way valve disposed between the transfer channel, the injection channel, and the evacuation channel and selectively operable to establish fluid communication between the evacuation channel and the injection channel, between the evacuation channel and the transfer channel, and between the transfer channel and the injection channel.

18. The adhesive injection apparatus of claim 17 , further comprising:
the adhesive reservoir.

19. The adhesive injection apparatus of claim 18 , wherein the adhesive reservoir contains a de-aerated adhesive.

20. The adhesive injection apparatus of claim 18 , further comprising:
a frangible seal separating the adhesive reservoir from the transfer channel.

Assignees

• Boeing Co

Inventors

• Hafenrichter Joseph L
• Georgeson Gary E
• Piehl Marc J

Classifications

• B29C73/025 Primary

  fed under pressure · CPC title

• B29C73/24

  Apparatus or accessories not otherwise provided for · CPC title

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C73/10

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

• B29C65/542

  by injection · CPC title