Co-curing process for the joining of composite structures

Patent metadata

Field	Value
Publication number	US-9731453-B2
Application number	US-201514639112-A
Country	US
Kind code	B2
Filing date	Mar 4, 2015
Priority date	Mar 4, 2015
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A method of fabricating a composite assembly may include providing a first laminate and a second laminate respectively formed of first and second composite plies, and having a respective first and second cured section and a respective first and second uncured section. The method may further include interleaving the first composite plies in the first uncured section with the second composite plies in the second uncured section to form an interfacial region. The method may additionally include curing the interfacial region to join the first laminate to the second laminate and form a unitized composite assembly.

First claim

What is claimed is:

1. A method of fabricating a composite assembly, including:
providing a first laminate and a second laminate respectively formed of first and second composite plies and having a respective first and second cured section and a respective first and second uncured section;
interleaving at least one of the first composite plies in the first uncured section with the second composite plies in the second uncured section to form an interfacial region, the interleaving of the at least one of the first composite plies with the second composite plies forming an interleaved ply;
laying up one or more splice plies over the interleaved ply in the interfacial region, the splice plies being different plies from those of the first laminate and the second laminate; and
curing the interfacial region to join the first laminate to the second laminate and form a unitized composite assembly.

2. The method of claim 1 , wherein the step of interleaving includes:
inserting at least one of the first composite plies in the first uncured section between a pair of immediately adjacent second composite plies in the second uncured section.

3. The method of claim 1 , wherein the step of curing the interfacial region includes:
heating the interfacial region; and
wherein the heating of the first and second cured section is less than the heating of the interfacial region when heating the interfacial region.

4. The method of claim 1 , wherein the step of interleaving includes:
at least partially overlapping at least one of the first composite plies of the first uncured section with at least one of the second composite plies of the second uncured section to form the interfacial region.

5. The method of claim 1 , wherein the step of interleaving includes:
staggering at least two ply joints joining the first and second laminate.

6. The method of claim 1 , wherein the first composite plies and the second composite plies each include at least one 0-degree ply, the step of interleaving including:
overlapping a 0-degree ply in the first uncured section of the first laminate with a 0-degree ply in the second uncured section of the second laminate to form an overlap joint.

7. The method of claim 1 , wherein the first composite plies and the second composite plies each include at least one non-0-degree ply, the step of interleaving including:
butting a non-0-degree ply in the first uncured section of the first laminate with a non-0-degree ply in the second uncured section of the second laminate to form a butt joint.

8. The method of claim 1 , wherein the step of interleaving includes:
interleaving an additional uncured section of at least one additional layup with the first and second uncured section to form the interfacial region.

9. The method of claim 1 , wherein the step of laying up one or more splice plies includes:
overlapping at least one of the splice plies over a ply end of at least one of the first composite plies and over a ply end of at least one of the second composite plies.

10. The method of claim 9 , wherein the step of laying up one or more splice plies includes:
laying up a plurality of splice plies over the first and second composite plies with a ramp rate of greater than 1:1.

11. The method of claim 1 , wherein the step of curing the interfacial region is performed using at least one of an autoclave, a press clave, an oven, and thermal blankets.

12. The method of claim 1 , wherein the step of curing the interfacial region comprises:
supporting the interfacial region on interfacial region cure tool, a remainder of at least a portion of the first laminate and the second laminate being unsupported by the interfacial region cure tool.

13. The method of claim 1 , wherein at least one of the composite plies in the first and second laminates is a non-0-degree ply or a non-90-degree ply formed of unidirectional tape and forming a crenulated edge in the respective first and second uncured section, the step of interleaving including:
inserting a tape end of the unidirectional tape of a first composite ply between a pair of the second composite plies.

14. A method of fabricating a composite assembly, including:
laying up a plurality of first composite plies to form a first layup;
laying up a plurality of second composite plies to form a second layup;
inserting a ply separator between at least one pair of the first composite plies and/or between at least one pair of the second composite plies;
at least partially curing the respective first and second layup to form a respective first and second cured section and a respective first and second uncured section containing the ply separator between the at least one pair of the first composite plies and/or between the at least one pair of the second composite plies;
preventing, due to insertion of the ply separator, bonding between the at least one pair of the first composite plies and/or between the at least one pair of the second composite plies during the at least partial curing of the respective first and second cured section;
removing, after the at least partial curing, the ply separator from between the at least one pair of the first composite plies and/or from between the at least one pair of the second composite plies;
interleaving the first composite plies in the first uncured section with the second composite plies in the second uncured section to form an interfacial region;
and
curing the interfacial region to join the first layup to the second layup and form a unitized composite assembly.

15. The method of claim 14 , wherein the steps of curing the first and second layup include:
heating a respective portion of the first and second layup defining the respective first and second cured section; and
wherein the heating of the portion of the first and second layup defining the first and second uncured section is less than the heating of the first and second cured section when heating the respective portion of the first and second layup defining the respective first and second cured section.

16. The method of claim 14 , wherein the steps of curing the first and second layup include:
partially curing at least one of the first and second uncured sections to a partial cure state of less than approximately 10 percent.

17. The method of claim 16 , wherein the step of partially curing includes:
partially curing at least one of the first and second uncured sections such that tack is reduced.

18. A method of fabricating a composite assembly, including:
laying up a plurality of first composite plies and a plurality of second composite plies to respectively form a first layup and a second layup;
curing to full cure a first cured section and a second cured section of the respective first and second layup;
partially curing to approximately 5 percent a first uncured section and a second uncured section of the respective first and second layup;
interleaving at least one of the first composite plies in the first uncured section between a pair of second composite plies in the second uncured section to form an interfacial region, the interleaving of the at least one of the first composite plies with the second composite plies forming an interleaved ply;
laying up one or more splice plies over the interleaved ply in the interfacial region, the splice plies being different plies from those of the first layup and the second layup; and
curing the interfacial region to form a unitized composite assembly.

19. The method of claim 1 , wherein the step of curing the interfa

Assignees

• Boeing Co

Inventors

• Humfeld Keith D
• Nelson Karl M

Classifications

• B29C66/61

  Joining from or joining on the inside (for making tubes by bending sheets and joining from the inside B29C53/387) · CPC title

• B29C66/131

  Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area · CPC title

• B29C65/505

  and placed in a recess formed in the parts to be joined, e.g. in order to obtain a continuous surface · CPC title

• B29C66/721

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

• B29C66/112

  Single lapped joints · CPC title