IP Library Granted Patent US 7,192,504
Granted Patent B2
US 7,192,504 · App. 10/476,074 · Granted Mar 20, 2007

Adding glass to composite bonding surfaces

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Quick Facts
Patent No.
US 7,192,504
App. No.
10/476,074
Granted
Mar 20, 2007
Kind
B2
Abstract

The present invention relates to a method of bonding together two pieces of composite material ( 10, 26 ) by applying a layer of glass fibre ( 20, 28 ) to a surface of each piece of composite material 10, 26 , and bonding the pieces together by means of adhesive ( 30 ) between the layers of glass fibre ( 10, 26 ). The inclusion of the glass fibre layers ( 20, 28 ) advantageously promotes failure of the bond adjacent the glass fibre-adhesive interface rather than at the glass fibre-composite material interface, with the result that damage to the composite material ( 10, 26 ) is minimised, and subsequent repair is made easier.

Claims (28)

1. A method of bonding together two pieces of composite material, the method comprising the steps of:

first, applying a layer of glass fibre to a surface of each piece of composite material; and

second, bonding the pieces together by means of adhesive between the layers of glass fibre, whereby in the event of failure in the joint, such failure is likely to occur adjacent the adhesive/glass fibre interface and hence minimise damage to the composite material.

2. A method according to claim 1 , wherein lay-up of the layer of glass fibres is transverse to the outer layer of fibres of the composite material.

3. A method according to claim 2 , wherein lay-up of the layer of glass fibres is aligned +/−45 degrees to the outer layer of fibres of the composite material.

4. A method according to claim 1 , wherein a plurality of layers of glass fibre are used.

5. A method according to claim 4 , wherein the layers of glass fibres are in the form of a fabric.

6. A method according to claim 1 , wherein the or each layer of glass fibre is co-cured onto the surfaces of the pieces of composite material.

7. A method according to claim 1 , wherein the adhesive is a film adhesive.

8. A method according to claim 1 , wherein the adhesive is a paste adhesive.

9. A method according to claim 1 , wherein the adhesive is applied such that it forms a layer which is between 0.05 mm and 2.5 mm thick.

10. A method according to claim 9 , wherein the adhesive layer is between 0.2 mm and 1 mm thick.

11. A method according to claim 1 , wherein the method further includes the step of grit blasting, washing and drying the bonding surface of glass fibre layers prior to the application of the adhesive thereto.

12. A composite joint produced according to the method of claim 1 .

13. A method of bonding together two pieces of composite material, the method comprising the steps of:

first, applying a layer of glass fibre to an opposing surface of each piece of composite material; and

second, bonding the opposing surfaces of the pieces together by means of adhesive between the layers of glass fibre, whereby in the event of failure in the joint, such failure is likely to occur adjacent the adhesive/glass fibre interface and hence minimise damage to the composite material.

14. A method according to claim 13 , wherein lay-up of the layer of glass fibres is transverse to the outer layer of fibres of the composite material.

15. A method according to claim 14 , wherein lay-up of the layer of glass fibres is aligned +/−45 degrees to the outer layer of fibres of the composite material.

16. A method according to claim 13 , wherein a plurality of layers of glass fibre are used.

17. A method according to claim 16 , wherein the layers of glass fibres are in the form of a fabric.

18. A method according to claim 13 , wherein the or each layer of glass fibre is co-cured onto the surfaces of the pieces of composite material.

19. A method according to claim 13 , wherein the adhesive is a film adhesive.

20. A method according to claim 13 , wherein the adhesive is a paste adhesive.

21. A method according to claim 13 , wherein the adhesive is applied such that it forms a layer which is between 0.05 mm and 2.5 mm thick.

22. A method according to claim 21 , wherein the adhesive layer is between 0.2 mm and 1 mm thick.

23. A method according to claim 13 , wherein the method further includes the step of grit blasting, washing and drying the bonding surface of glass fibre layers prior to the application of the adhesive thereto.

24. A composite joint produced according to the method of claim 13 .

Assignments (3)
CHANGE OF NAME Recorded Apr 18, 2011
From: AIRBUS UK LIMITED
To: AIRBUS OPERATIONS LIMITED
Reel/Frame 026141/0311 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 11, 2005
From: BAE SYSTEMS PLC
To: AIRBUS UK LIMITED
Reel/Frame 016547/0416 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 28, 2003
From: HEALEY, MICHAEL JOHN
To: BAE SYSTEMS PLC
Reel/Frame 015276/0545 →