IP Library › Granted Patent US 10,022,922
Granted Patent B2
US 10,022,922 · App. 14/335,269 · Granted Jul 17, 2018

Bonded patches with bond line control

Inventors: Steven Donald Blanchard (Issaquah, WA); Aydin Akdeniz (Langley, WA); John Spalding (Renton, WA); David M. Anderson (Sammamish, WA); Michael W. Evens (Burien, WA)
Assignee: The Boeing Company
B29C73/10B29C65/18B29C65/247B29C65/4835B29C65/4875B29C65/526B29C65/7826B29C66/1122B29C66/45B29C66/472B29C66/91218B29C66/91231B29C66/91421B29C66/961B29C73/12C09J5/00C09J5/06B29C35/02B29C65/524B29C66/721B29C66/8322B29K2105/06B29K2105/16B29L2031/3076
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Quick Facts
Patent No.
US 10,022,922
App. No.
14/335,269
Granted
Jul 17, 2018
Kind
B2
Abstract

A patch may be used to rework a composite structure in the field. The patch is bonded to the structure by a layer of adhesive and includes perforations that allow the escape of air from the adhesive as the patch is compressed against the structure. A spacer may be introduced between the patch and the structure to control the thickness of the adhesive layer.

Claims (53)

1. A method of bonding a patch on structure, comprising:

placing the patch on the structure;

placing a layer of bonding adhesive between the patch and the structure;

placing a caul plate over the patch;

pressing the patch against the structure by applying pressure to the caul plate;

using an anti-caul plate to limit the pressure applied to a periphery of the patch by the caul plate; and

placing a non-reversible temperature indication strip on the anti-caul plate.

2. The method of claim 1 , further comprising:

placing a heat pack over the anti-caul plate, the nonreversible temperature indication strip, and the patch.

3. The method of claim 2 further comprising:

activating the heat pack to produce heat.

4. The method of claim 2 further comprising:

prior activating the heat pack, measuring a preactivation temperature of the heat pack with a first reversible temperature indication strip; and

raising the pre-activation temperature if the preactivation temperature is less than a desired temperature.

5. The method of claim 4 further comprising:

activating the heat pack; and

measuring a second temperature of the heat pack with a second, different reversible temperature indication strip.

6. The method of claim 5 further comprising:

if the second temperature fails to reach a second desired temperature, taking an action to increase the second temperature.

7. The method of claim 6 wherein the action comprises replacing the heat pack with a second heat pack and activating the second heat pack.

8. The method of claim 1 , wherein limiting the pressure applied to the periphery of the patch includes a reacting force applied to the caul plate around a perimeter of the caul plate.

9. The method of claim 1 , wherein the reacting force includes placing an anti-caul plate between the caul plate and the structure at the perimeter of the caul plate.

10. The method of claim 1 , further comprising:

placing a spacer between the patch and the structure to maintain the layer of bonding adhesive at a desired thickness.

11. The method of claim 10 , wherein placing a spacer between the patch and the structure includes introducing beads into the adhesive, each of the beads having a dimension generally equal to the desired thickness of the layer of bonding adhesive.

12. The method of claim 10 , wherein placing a spacer between the patch and the structure includes introducing a screen between the patch and the structure having a thickness generally equal to the desired thickness of the layer of bonding adhesive.

13. Apparatus for adhesively bonding a patch on a structure surface, comprising:

a caul plate adapted to be placed on and apply pressure to the patch during a bonding operation; and

an anti-caul plate between the caul plate and the structure surface, the anti-caul plate configured to limit an applied pressure to a periphery of the patch by the caul plate; and

a non-reversible temperature indication strip on the anti-caul plate.

14. The apparatus of claim 13 further comprising:

a heat pack placed over the anti-caul plate.

15. The apparatus of claim 14 further comprising:

a first temperature indicator strip on the heat pack and configured to indicate a pre-activation temperature of the heat pack; and

a second temperature indicator strip on the heat pack and configured to indicate an activated temperature of the heat pack.

16. The apparatus of claim 13 , wherein the anti-caul plate substantially surrounds the patch.

17. The apparatus of claim 13 , wherein:

the anti-caul plate is substantially circular and circumscribes the patch, and a perimeter of the caul plate overlies and engages the anti-caul plate.

18. A method of reworking a composite aircraft structure in the field, comprising:

preparing an area of the structure to be reworked;

forming a patch including forming perforations in the patch;

applying a layer of adhesive to one of the patch and the structure;

controlling a thickness of the adhesive layer by placing a spacer between the patch and the structure;

applying the patch to the structure;

placing a caul plate over the patch;

placing an anti-caul plate between the caul plate and the structure;

placing a non-reversible temperature indication strip on the anti-caul plate;

installing a pressure applicator over the combination of the patch, the caul plate and the anti-caul plate;

using the pressure applicator to apply pressure to the patch through the caul plate;

using the anti-caul plate to limit the pressure applied by the caul plate to a periphery of the patch;

installing a heat pack over the patch; and

using the heat pack to cure the adhesive.

19. The method of claim 11 , wherein placing a spacer between the patch and the structure also includes introducing a screen together with the beads between the patch and the structure, the screen and the beads both having a thickness generally equal to the desired thickness of the layer of bonding adhesive.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 18, 2014
From: BLANCHARD, STEVEN DONALD; AKDENIZ, AYDIN; SPALDING, JOHN; ANDERSON, DAVID M.; EVENS, MICHAEL W.
To: THE BOEING COMPANY
Reel/Frame 033344/0435 →
Continuity (3)
Continuation In Part 12554554 · Sep 4, 2009
Continuation In Part 12328903 · Dec 5, 2008
Related Publication 20140326389A1 · Nov 6, 2014