Composite duct with reinforcement

Patent metadata

Field	Value
Publication number	US-10823449-B2
Application number	US-201816003823-A
Country	US
Kind code	B2
Filing date	Jun 8, 2018
Priority date	Jun 8, 2018
Publication date	Nov 3, 2020
Grant date	Nov 3, 2020

Abstract

A composite duct with reinforcement comprises an inner ply, an outer ply, and a plurality of cellular core rings. The inner ply forms a channel with a circular cross-section. The plurality of cellular core rings is positioned at set intervals along a length of the composite duct and between the inner ply and the outer ply.

First claim

What is claimed is:

1. A method of forming a composite duct with reinforcement comprising:
forming a first ply into a tube with a circular cross-section;
positioning a partial ply and a cellular core ring over a portion of the first ply, wherein the cellular core ring is formed of a cellular core strip having bevels; and
laying up a second ply over the partial ply and the cellular core ring to form the composite duct with reinforcement.

2. The method of claim 1 , wherein positioning the partial ply and the cellular core ring over the portion of the first ply comprises wrapping the strip of cellular core around the circular cross-section and applying the partial ply over the strip of cellular core.

3. The method of claim 2 , wherein the strip of cellular core has a first face and a second face opposite the first face, wherein the second face has the bevels, and wherein wrapping the strip of cellular core comprises wrapping the strip of cellular core such that the first face contacts the first ply.

4. The method of claim 3 , wherein each of the bevels has a length of ¼ inch to 1 inch.

5. The method of claim 1 , wherein positioning the partial ply and the cellular core ring over the portion of the first ply comprises wrapping the partial ply around the circular cross-section and applying the strip of cellular core over the partial ply.

6. The method of claim 5 , wherein the strip of cellular core has a first face and a second face opposite the first face, wherein the second face has the bevels, and wherein applying the strip of cellular core over the partial ply comprises applying the strip of cellular core such that the first face contacts the partial ply.

7. The method of claim 1 further comprising:
positioning a second partial ply and a second cellular core ring over a second portion of the first ply, wherein the second cellular core ring is a set distance away from the cellular core ring.

8. The method of claim 7 , wherein the set distance is in the range of 10 inches to 25 inches.

9. The method of claim 1 , wherein positioning the partial ply and the cellular core ring over the portion of the first ply comprises positioning the cellular core ring such that centerlines of cells of the cellular core ring are perpendicular to a surface of the first ply.

10. The method of claim 1 , wherein the cellular core ring has a trapezoidal cross-section.

11. The method of claim 1 , wherein the cellular core ring is formed of a honeycomb material having a thickness in the range of 1/16 inch to ½ inch.

12. The method of claim 1 , wherein the cellular core ring is formed of a honeycomb material having a width in the range of 1 inch to 3 inches.

13. A method of forming a composite duct with reinforcement comprising:
forming a first ply into a tube with a circular cross-section;
positioning a plurality of cellular core rings around the circular cross-section, the plurality of cellular core rings separated by set intervals;
positioning a second ply over the plurality of cellular core rings; and
curing the first ply and second ply to form the composite duct with reinforcement;
wherein the plurality of cellular core rings each is formed of a respective cellular core strip having bevels.

14. The method of claim 13 , wherein the plurality of cellular core rings each is formed of a honeycomb material having a thickness in the range of 1/16 inch to ½ inch.

15. The method of claim 13 , wherein the bevels each have a length in the range of ¼ inch to 1 inch.

16. The method of claim 13 further comprising:
placing a plurality of partial plies around the circular cross-section, wherein positioning the second ply over the plurality of cellular core rings comprises positioning the second ply over the plurality of partial plies.

17. A method of forming a composite duct with reinforcement comprising:
forming a first ply into a tube with a circular cross-section;
positioning a partial ply and a cellular core ring over a portion of the first ply, wherein the cellular core ring has a trapezoidal cross-section; and
laying up a second ply over the partial ply and the cellular core ring to form the composite duct with reinforcement.

18. The method of claim 17 , wherein positioning the partial ply and the cellular core ring over the portion of the first ply comprises wrapping a strip of cellular core around the circular cross-section and applying the partial ply over the strip of cellular core.

19. The method of claim 17 , wherein positioning the partial ply and the cellular core ring over the portion of the first ply comprises wrapping a partial ply around the circular cross-section and applying a strip of cellular core over the partial ply.

20. The method of claim 17 further comprising:
positioning a second partial ply and a second cellular core ring over a second portion of the first ply, wherein the second cellular core ring is a set distance away from the cellular core ring.

Assignees

• Boeing Co

Inventors

• Maben Douglas Dean
• Perdoch Johnathan
• Cox Jennifer Fiore
• Saldana Altagracia

Classifications

• B29D24/007

  and a chamfered edge · CPC title

• B32B3/20

  of hollow pieces, e.g. tubes; of pieces with channels or cavities · CPC title

• B32B2605/18

  Aircraft · CPC title

• B32B5/12

  characterised by the relative arrangement of fibres or filaments of {different layers, e.g. the fibres or filaments being parallel or perpendicular to each other} · CPC title

• B32B2307/558

  Impact strength, toughness · CPC title