Systems and methods for curing complex fiber-reinforced composite structures

Patent metadata

Field	Value
Publication number	US-9827697-B2
Application number	US-201414473184-A
Country	US
Kind code	B2
Filing date	Aug 29, 2014
Priority date	Aug 29, 2014
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

Systems and methods for curing complex fiber-reinforced composite structures utilize two distinct heat sources. A first heat source is utilized for heating a complex fiber-reinforced composite structure from within an internal portion of the complex fiber-reinforced composite structure. A second heat source is utilized for heating the complex fiber-reinforced composite structure from an external surface of the complex fiber-reinforced composite structure.

First claim

The invention claimed is:

1. A method for curing complex fiber-reinforced composite structures, the method comprising:
applying heat from a first heat source to an internal portion of a complex fiber-reinforced composite structure for conductive heating of the complex fiber-reinforced composite structure from the internal portion, wherein the internal portion includes heat conductive fibers, and wherein the applying heat from the first heat source includes contacting exposed ends of the heat conductive fibers with the first heat source for conduction along lengths of the heat conductive fibers within the internal portion for conductive heating of the complex-fiber reinforced composite structure from the internal portion; and
applying heat from a second heat source distinct from the first heat source to an external surface of the complex fiber-reinforced composite structure for conductive heating of the complex fiber-reinforced composite structure from the external surface.

2. The method of claim 1 , further comprising:
following the applying heat from the first heat source, actively withdrawing heat with a heat sink from the internal portion of the complex fiber-reinforced composite structure to cool the complex fiber-reinforced composite structure from within the internal portion.

3. The method of claim 2 , wherein the first heat source and the heat sink share structure for applying heat to and withdrawing heat from the internal portion of the complex fiber-reinforced composite structure.

4. The method of claim 1 , wherein the second heat source includes one of an autoclave and an oven with an internal volume sized to receive the complex fiber-reinforced composite structure.

5. The method of claim 1 , wherein the second heat source includes one or more heating pads or blankets configured to engage the external surface.

6. The method of claim 1 , wherein the complex fiber-reinforced composite structure includes at least two regions having different physical characteristics from each other, and wherein the internal portion of the complex fiber-reinforced composite structure defines at least a portion of an interface between the at least two regions, and wherein the different physical properties includes one or more of different fiber material, different fiber orientation, different fiber size, different fiber density, different resin material, different layer thickness, different layer orientation, and different coefficient of thermal expansion.

7. The method of claim 1 , wherein the complex fiber-reinforced composite structure includes at least two regions having different thermal characteristics from each other, and wherein the internal portion of the complex fiber-reinforced composite structure includes one of the at least two regions.

8. The method of claim 1 , wherein the complex fiber-reinforced composite structure includes at least one interface between two regions, wherein the interface creates a thermal discontinuity between the two regions, and wherein the internal portion of the complex fiber-reinforced composite structure includes one of the two regions.

9. The method of claim 1 , wherein the internal portion of the complex fiber-reinforced composite structure is a radius filler.

10. The method of claim 1 , wherein the complex fiber-reinforced composite structure includes at least two sheets of fiber-reinforced composite material and a radius filler of fiber-reinforced composite material positioned between the at least two sheets, and wherein the internal portion of the complex fiber-reinforced composite structure is the filler.

11. The method of claim 1 , wherein the complex fiber-reinforced composite structure includes a plurality of layers of fiber-reinforced composite material, and wherein the internal portion of the complex fiber-reinforced composite structure is at least one layer of the plurality of layers.

12. The method of claim 1 , wherein the complex fiber-reinforced composite structure includes one or more of a stringer, a stringer and skin assembly, a wing spar, a wing spar and skin assembly, a wing rib, a wing rib and spar assembly, a wing rib and skin assembly, a frame member, a frame member and skin assembly, and an assembly between more than one fiber-reinforced composite part.

13. The method of claim 1 , wherein the heat conductive fibers are constructed of a material different than fibers within a remainder of the complex fiber-reinforced composite structure.

14. The method of claim 1 , wherein the complex fiber-reinforced composite structure has a longitudinal axis, and wherein the heat conductive fibers are generally aligned with the longitudinal axis.

15. The method of claim 1 , wherein the applying heat from the first heat source is initiated prior in time to the applying heat from the second heat source.

16. The method of claim 15 , wherein the applying heat from the first heat source is ceased prior in time to ceasing the applying heat from the second heat source.

17. The method of claim 15 , wherein the applying heat from the first heat source is ceased prior to initiation of the applying heat with the second heat source.

18. The method of claim 1 , further comprising:
actively monitoring temperatures of one or more regions of the complex fiber-reinforced composite structure; and
based at least in part on the actively monitoring, actively controlling timing of the applying heat from the first heat source and the applying heat from a second heat source.

19. The method of claim 1 , further comprising:
withdrawing heat from the complex fiber-reinforced composite structure via the external surface concurrently with the applying heat from the first heat source and prior to the applying heat from the second heat source.

20. A method for curing complex fiber-reinforced composite structures, the method comprising:
applying heat from a first heat source to an internal portion of a complex fiber-reinforced composite structure having a longitudinal axis for conductive heating of the complex fiber-reinforced composite structure from the internal portion, wherein the internal portion includes heat conductive fibers generally aligned with the longitudinal axis, wherein the heat conductive fibers are constructed of a material different than fibers within a remainder of the complex fiber-reinforced composite structure, and wherein the applying heat from the first heat source includes contacting with the first heat source exposed ends of the heat conductive fibers for conduction along lengths of the heat conductive fibers within the internal portion for conductive heating of the complex fiber-reinforced composite structure from the internal portion; and
applying heat from a second heat source distinct from the first heat source to an external surface of the complex fiber-reinforced composite structure for conductive heating of the complex fiber-reinforced composite structure from the external surface, wherein the second heat source includes at least one of an autoclave, an oven, a heating pad, and a heating blanket.

21. The method of claim 1 , wherein the internal portion is encased within a remainder of the complex fiber-reinforced composite structure.

22. The method of claim 1 , wherein, in cross-section, the internal portion is surrounded by and in contact with a remainder of the complex fiber-reinforced composite structure.

Assignees

• Boeing Co

Inventors

• Tien Allan
• Souksamrane Samson
• Apdalhaliem Sahrudine

Classifications

• B29C35/02

  Heating or curing, e.g. crosslinking or vulcanizing {during moulding, e.g. in a mould}(cold vulcanisation B29C35/18 {; vulcanising tyres, presses therefor B29D30/0601}) · CPC title

• B29C35/0272

  using lost heating elements, i.e. heating means incorporated and remaining in the formed article (for preforms with internal stresses B29C61/0625; joining using lost heating elements B29C65/34; making electrically conductive articles B29C70/882) · CPC title

• B29C35/0227

  using pressure vessels, e.g. autoclaves, vulcanising pans (B29C35/065 takes precedence) · CPC title

• B29C35/0288

  Controlling heating or curing of polymers during moulding, e.g. by measuring temperatures or properties of the polymer and regulating the process (controlling or regulating chemical, physical or physico- chemical processes in general B01J19/0006) · CPC title

• B29K2105/08

  of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns · CPC title