Composite laminate structures

Patent metadata

Field	Value
Publication number	US-11220069-B2
Application number	US-201916719903-A
Country	US
Kind code	B2
Filing date	Dec 18, 2019
Priority date	Sep 24, 2017
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

Composite laminate structures are produced using partially cured parts. Partial curing of the parts is achieved by applying a catalyst to regions of the parts that are to be fully cured. These regions cure at a lower-than-normal temperature while remaining regions of the part remain uncured, allowing them to be co-bonded or co-cured to other structures.

First claim

What is claimed is:

1. A composite laminate part layup, that comprises:
a first plurality of thermoset composite plies;
a second plurality of thermoset composite plies; and

an interfacial region defined within an overlapping area located between both the first plurality of thermoset composite plies and the second plurality of thermoset composite plies;
wherein a ply of the second plurality of thermoset composite plies comprises a resin curing accelerator located within a region of said ply located outside of the overlapping area;
wherein said ply does not have the resin curing accelerator within the overlapping area; and
wherein another ply of the second plurality of thermoset composite plies comprises the resin curing accelerator located within the overlapping area, such that the second plurality of thermoset composite plies comprises the resin curing accelerator in only a subset of plies within the thickness of the overlapping area in the second plurality of thermoset composite plies.

2. The composite laminate part layup of claim 1 , wherein the second plurality of thermoset composite plies comprises at least one ply having the resin curing accelerator applied across an entirety of the at least one ply.

3. The composite laminate part layup of claim 1 , wherein the first plurality of thermoset composite plies comprises the resin curing accelerator applied across an entirety of each ply of the first plurality of thermoset composite plies.

4. The composite laminate part layup of claim 1 , wherein the interfacial region is configured to be co-cured in a lap joint.

5. The composite laminate part layup of claim 1 , wherein a resin in the first plurality of thermoset composite plies comprises at least one of: epoxy resin, cyanate ester resin, polyurethane resin, or phenolic resin.

6. The composite laminate part layup of claim 1 , wherein all of the first plurality of thermoset composite plies are thermoset pre-preg plies.

7. The composite laminate part layup of claim 3 , wherein the first plurality of thermoset composite plies further comprises a stabilizer to prevent potential degradation of the resin curing accelerator.

8. The composite laminate part layup of claim 1 , wherein the first plurality of thermoset composite plies comprises cured portions.

9. The composite laminate part layup of claim 1 , wherein the interfacial region is configured to be co-cured in a scarf joint.

10. The composite laminate part layup of claim 1 , wherein a resin in the second plurality of thermoset composite plies comprises at least one of: epoxy resin, cyanate ester resin, polyurethane resin, or phenolic resin.

11. The composite laminate part layup of claim 1 , wherein all of the second plurality of thermoset composite plies are thermoset pre-preg plies.

12. The composite laminate part layup of claim 1 , wherein the second plurality of thermoset composite plies further comprises a stabilizer to prevent potential degradation of the resin curing accelerator.

13. The composite laminate part layup of claim 1 , wherein the second plurality of thermoset composite plies further comprises cured portions.

14. A composite laminate part layup, that comprises:
a plurality of thermoset composite plies comprising a region,
wherein a ply of the plurality of thermoset composite plies comprises a resin curing accelerator located outside of the region,
wherein said ply does not have an application of the resin curing accelerator within the region, and
wherein another ply of the plurality of thermoset composite plies comprises the resin curing accelerator located within the region, such that the plurality of thermoset composite plies comprises the resin curing accelerator in only a subset of plies of the plurality of thermoset composite plies within the thickness of the region.

15. The composite laminate part layup of claim 14 , wherein at least one ply of the plurality of thermoset composite plies comprises the resin curing accelerator applied across an entirety of the at least one ply.

16. The composite laminate part layup of claim 14 , wherein a resin in the plurality of thermoset composite plies comprises at least one of: epoxy resin, cyanate ester resin, polyurethane resin, or phenolic resin.

17. The composite laminate part layup of claim 14 , wherein all of the plurality of thermoset composite plies are thermoset pre-preg plies.

18. The composite laminate part layup of claim 14 , wherein the plurality of thermoset composite plies further comprises a stabilizer to prevent potential degradation of the resin curing accelerator.

19. The composite laminate part layup of claim 14 , wherein the plurality of thermoset composite plies further comprises pre-cured portions.

20. The composite laminate part layup of claim 1 , wherein said ply is uncured in the overlapping area and cured outside of the overlapping area, and wherein said another ply is cured in the overlapping area such that the second plurality of thermoset composite plies comprises at least one cured ply and at least one uncured ply within the thickness of the overlapping area in the second plurality of thermoset composite plies.

21. The composite laminate part layup of claim 14 , wherein said ply is uncured in the region and cured outside of the region, and wherein said another ply is cured in the region such that the plurality of thermoset composite plies comprises at least one cured ply and at least one uncured ply within the thickness of the region in the plurality of thermoset composite plies.

Assignees

• Boeing Co

Inventors

• Ogale Amol

Classifications

• B29C35/0266 Primary

  Local curing (for repairing B29C73/34) · CPC title

• B29C70/304

  In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining · CPC title

• B29C66/112

  Single lapped joints · CPC title

• B29C66/73941

  characterised by the materials of both parts being thermosets · CPC title

• B29C66/721

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title