Manufacture of a resin infused one-piece composite truss structure

Patent metadata

Field	Value
Publication number	US-10272619-B2
Application number	US-201414281305-A
Country	US
Kind code	B2
Filing date	May 19, 2014
Priority date	May 19, 2014
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

A composite truss structure may have a first facesheet, a second facesheet, and a plurality of truss elements joined with the first facesheet and the second facesheet at nodes to form a one-piece structure. The composite truss structure may be formed by a method comprising preparing a dry fabric mold by: 1) placing a first dry fabric layer on a tool, 2) placing a first layer of fabric-loaded mandrels on the first dry fabric layer, 3) placing a second layer of the fabric-loaded mandrels on the first layer of fabric-loaded mandrels, and 4) placing a second dry fabric layer over the fabric-loaded mandrels. The method may further comprise infusing the dry fabric mold with a resin, and curing the resin to provide the nonflexible composite truss structure.

First claim

What is claimed is:

1. A method for fabricating a composite truss structure having a core with a plurality of truss elements, comprising:
preparing a dry fabric mold by a method comprising
placing a first dry fabric layer on a tool having a non-corrugated surface, and
placing a first layer of fabric-loaded mandrels on the first dry fabric layer to create a corrugated surface, each of the fabric-loaded mandrels having a major axis and including a dry fabric tube wrapped around a mandrel, the first layer of fabric-loaded mandrels including a row of the fabric-loaded mandrels aligned in abutment and in parallel along the major axes of the fabric-loaded mandrels, each of the fabric-loaded mandrels of the row having a same cross-sectional shape that becomes progressively smaller across the row to provide a wedge structure;

infusing the dry fabric mold with a resin;
curing the resin to provide the composite truss structure; and
repeatedly slicing the composite truss structure along an axis perpendicular to the major axes to provide a plurality of individual components each having the composite truss structure.

2. The method of claim 1 , wherein preparing the dry fabric mold further comprises placing a second layer of fabric-loaded mandrels on the first layer of fabric-loaded mandrels by positioning each of the fabric-loaded mandrels of the second layer in a respective one of grooves formed on the corrugated surface, the second layer of fabric-loaded mandrels including a second row of the fabric-loaded mandrels aligned in abutment and in parallel along the major axes of the fabric-loaded mandrels, each of the fabric-loaded mandrels of the second row having a same cross-sectional shape that becomes progressively smaller across the second row to provide the wedge structure.

3. The method of claim 2 , wherein preparing the dry fabric mold further comprises placing a second dry fabric layer over the second layer of fabric-loaded mandrels.

4. The method of claim 3 , further comprising preparing each of the fabric-loaded mandrels by pulling the dry fabric tube over the mandrel or by braiding the dry fabric tube over the mandrel.

5. The method of claim 3 , further comprising removing the mandrels from the composite truss structure after curing the resin to provide the composite truss structure.

6. The method of claim 5 , wherein removing the mandrels from the composite truss structure comprises treating the mandrels with a solvent.

7. The method of claim 5 , wherein preparing the dry fabric mold further comprises inserting a filler material in each gap in the dry fabric mold.

8. The method of claim 5 , wherein each of the fabric-loaded mandrels has a top and a base, and wherein placing the first layer of fabric-loaded mandrels on the first dry fabric layer comprises placing the base of each of the fabric-loaded mandrels in contact with the first dry fabric layer.

9. The method of claim 8 , wherein placing the second layer of fabric-loaded mandrels on the first layer of fabric-loaded mandrels comprises placing the top of each of the fabric-loaded mandrels of the second layer in contact with a bottom of a respective one of the grooves formed on the corrugated surface.

10. The method of claim 1 , wherein preparing the dry fabric mold further comprises:
placing additional layers of fabric-loaded mandrels over the first layer of fabric-loaded mandrels; and
placing a plurality of dry fabric layers at desired locations between the layers of fabric-loaded mandrels.

11. The method of claim 1 , wherein repeatedly slicing the composite truss structure along an axis parallel to the major axes to provide a plurality of individual components each having the composite truss structure comprises repeatedly slicing the entire composite truss structure into the plurality of individual components.

12. A method for fabricating a number of individual components each having a nonflexible composite truss structure formed from a fiber-reinforced resin material and having a first facesheet, a second facesheet, and a reinforcing core of truss elements fused with the first facesheet and the second facesheet, the method comprising:
preparing a dry fabric mold by a method comprising
placing a first dry fabric layer on a tool,
placing a first layer of fabric-loaded mandrels on the first dry fabric layer to create a corrugated surface having a plurality of grooves,
placing a second layer of fabric-loaded mandrels on the first layer of fabric-loaded mandrels by positioning each of the fabric-loaded mandrels of the second layer in a respective one of the grooves of the corrugated surface, each of the fabric-loaded mandrels of the first layer and the second layer having a major axis and including a dry fabric tube wrapped around a mandrel, each of the first layer and the second layer including a row of the fabric-loaded mandrels aligned in abutment and in parallel along the major axes of the fabric-loaded mandrels, each of the fabric-loaded mandrels of the row having a same cross-sectional shape that becomes progressively smaller across the row to provide a wedge structure, and
placing a second dry fabric layer over the fabric-loaded mandrels;

infusing the dry fabric mold with a resin;
curing the resin to provide a larger panel having the composite truss structure, the larger panel being sized to provide the number of individual components; and
repeatedly slicing the larger panel along an axis perpendicular to the major axes to provide the number of individual components each having the nonflexible composite truss structure.

13. The method of claim 12 , wherein each of the fabric-loaded mandrels include a top and a base that is wider than the top, and wherein placing the first layer of fabric-loaded mandrels on the first dry fabric layer further comprises aligning the fabric-loaded mandrels in parallel on the first dry fabric layer with the base of each fabric-loaded mandrel contacting the first dry fabric layer.

14. The method of claim 13 , wherein placing the second layer of fabric-loaded mandrels on the first layer of fabric-loaded mandrels further comprises inserting the top of each of the fabric-loaded mandrels of the second layer into a respective one of the grooves of the corrugated surface.

15. The method of claim 14 , further comprising preparing each of the fabric-loaded mandrels by pulling the dry fabric tube over the mandrel.

16. The method of claim 14 , further comprising preparing each of the fabric-loaded mandrels by braiding the dry fabric tube over the mandrel.

17. The method of claim 14 , further comprising removing the mandrels from the composite truss structure after curing the resin.

18. The method of claim 17 , wherein removing the mandrels from the composite truss structure comprises treating the mandrels with a solvent.

19. The method of claim 17 , wherein the mandrels are water-soluble, and wherein removing the mandrels from the composite truss structure comprises treating the mandrels with water.

20. A method for fabricating a composite truss structure having a first facesheet, a second facesheet, and a reinforcing core of truss elements fused with the first facesheet and the second facesheet, the method comprising:
preparing a dry fabric mold by a method comprising
placing a first dry fabric layer on a flat tool,
aligning a first layer of fabric-loaded mandrels on the first dry fabric layer to provide a corrugated surface having a plurality of parallel grooves, each of the fabric-loaded mandrels having a major axis and includi

Assignees

• Boeing Co

Inventors

• Lockett Peter J
• Scarfe Manning J
• Glynn Andrew K
• Pook David A

Classifications

• B29C70/446 Primary

  Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames · CPC title

• B29D24/002

  formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled (totally filled B29D99/0021) · CPC title

• B29C70/545

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

• Y02T50/43

  Cross-Sectional Technologies · mapped topic

• B29C70/44 Primary

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title