Structural integrated repair method and system tool device for repairing delaminated composite structures

Patent metadata

Field	Value
Publication number	US-9434139-B2
Application number	US-201414267052-A
Country	US
Kind code	B2
Filing date	May 1, 2014
Priority date	May 1, 2014
Publication date	Sep 6, 2016
Grant date	Sep 6, 2016

Abstract

A system for repair of damaged holes in composite structures incorporates a repair system tool device having a sleeve sized to be closely received in a hole in a composite structure. The sleeve has a central bore for receiving parent resin and an array of orifices for radial expulsion of the parent resin into the hole. A caul plate seals the central bore and a vacuum bag covering the caul plate is sealed to the surface of the composite structure. Introduction of vacuum in the vacuum bag provides a differential pressure for infusion of resin from the orifices in the sleeve into delaminations extending from the hole.

First claim

What is claimed is:

1. A system for repair of damaged holes in composite structures, said system comprising:
a repair system tool device having a sleeve sized to be closely received in a hole in a composite structure, said sleeve having a central bore for receiving parent resin and a selected array of orifices for radial expulsion of the parent resin into adjacent delaminations in the hole;
a caul plate sealing the central bore;
a vacuum bag covering the caul plate and sealed to a surface of the composite structure, wherein introduction of vacuum in the vacuum bag provides a differential pressure for infusion of resin from the orifices in the sleeve into delaminations extending from the hole.

2. The system for repair of damaged holes in composite structures as defined in claim 1 wherein the repair system tool device further comprises an upper flange from which the sleeve extends.

3. The system for repair of damaged holes in composite structures as defined in claim 2 further comprising a seal received around the sleeve adjacent the upper flange, said seal engaging a top surface of the structure around the hole.

4. The system for repair of damaged holes in composite structures as defined in claim 3 wherein the central bore of the sleeve is sealed opposite the upper flange.

5. The system for repair of damaged holes in composite structures as defined in claim 3 further comprising a lower flange engaging the sleeve opposite the upper flange and a seal received around the sleeve adjacent the lower flange, said seal engaging a bottom surface of the structure around the hole.

6. The system for repair of damaged holes in composite structures as defined in claim 5 wherein the sleeve incorporates a threaded end received in a mating threaded bore in the lower flange.

7. The system for repair of damaged holes in composite structures as defined in claim 1 wherein each of the orifices in the array of orifices has a diameter of between 0.01 and 0.1 inch.

8. The system for repair of damaged holes in composite structures as defined in claim 1 wherein the sleeve is titanium.

9. The system for repair of damaged holes in composite structures as defined in claim 1 wherein tubes are inserted in orifices in the selected array, said tubes extending beyond an outer surface of the sleeve.

10. The system for repair of damaged holes in composite structures as defined in claim 1 wherein plugs are inserted in orifices other than the selected array.

11. A method for repair of damage holes in composite structures, the method comprising:
conducting a non-destructive evaluation of a structural composite delaminated hole to assess damage;
inserting a repair system tool device sleeve having a plurality of orifices into the damaged delaminated hole;
introducing a predetermined amount of parent toughed resin into the sleeve of the repair system tool device through a central bore in the sleeve;
installing a caul plate and bagging for application of vacuum;
applying vacuum on the bag to urge the caul plate into sealing contact with a top flange maintaining substantially atmospheric pressure in the sleeve while placing a laminate around the hole under vacuum for diffusion of the resin through the orifices in the sleeve; and,
forcing the resin into the delaminations in the laminate surrounding the hole by capillary action.

12. The method as defined in claim 11 further comprising treating the sleeve of the repair system tool device with cetyle alcohol lubricant for installation.

13. The method as defined in claim 11 further comprising encircling the sleeve with an upper o-ring seal abutting the top flange.

14. The method as defined in claim 13 further comprising:
assembling a lower o-ring seal on the sleeve;
engaging a mating flange onto the sleeve; and,
tightening the mating flange to avoid leakage of resin.

15. The method as defined in claim 11 further comprising curing a damaged area under vacuum.

16. The method as defined in claim 15 further comprising:
unbagging a repaired area;
removing the caul plate; and,
withdrawing the repair system tool device sleeve from the hole.

17. The method as defined in claim 16 further comprising reaming the hole as repaired to remove excess resin and produce final tolerance hole size.

18. The method as defined in claim 17 further comprising installing a fastener into the repaired hole to continue with production.

19. The method as defined in claim 11 further comprising selecting an array of orifices to align with delaminations identified in the non-destructive evaluation.

20. The method as defined in claim 19 further comprising plugging orifices other than the selected array.

Assignees

• Boeing Co

Inventors

• Dan-Jumbo Eugene

Classifications

• B29C70/545 Primary

  Perforating, cutting or machining during or after moulding · CPC title

• B29C73/30

  for local pressing or local heating · CPC title

• B29C70/546

  Measures for feeding or distributing the matrix material in the reinforcing structure · CPC title

• B29C66/71

  characterised by the composition of the plastics material of the parts to be joined (welding bar compositions B29C65/125) · CPC title

• B29C65/544

  by suction · CPC title