Electrical curing of composite structures

Patent metadata

Field	Value
Publication number	US-10285219-B2
Application number	US-201514865833-A
Country	US
Kind code	B2
Filing date	Sep 25, 2015
Priority date	Sep 25, 2014
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

A composite structure cured by the process of: electrically coupling a first lead to a first portion of said composite structure; electrically coupling a second lead to a second portion of said composite structure; and using an electric power source to pass electric current through said composite structure from said first portion to said second portion, wherein passing said electric current through said composite structure causes the temperature of at least a portion of said composite structure increase to a predetermined temperature.

First claim

What is claimed is:

1. A composite structure cured by a process comprising the steps of:
electrically coupling a first lead to a first portion of the composite structure, wherein the composite structure comprises two layers of pre-impregnated carbon fiber 0° laminate material;
electrically coupling a second lead to a second portion of the composite structure;
passing an electric current through the composite structure from the first portion to the second portion using an electric power source to increase a temperature of a portion of the composite structure to a predetermined temperature; and
subjecting the composite structure to pressure using a vacuum when the electric current passes through the composite structure.

2. The composite structure of claim 1 , wherein a carbon nanotube material is positioned between the two layers of pre-impregnated carbon fiber 0° laminate material.

3. The composite structure of claim 1 , wherein an electrical contact is positioned between the two layers of pre-impregnated carbon fiber 0° laminate material at each of the first portion and the second portion to improve conductivity across the composite structure.

4. The composite structure of claim 1 , wherein the composite structure is laid up using a tool and cured while the composite structure is freestanding.

5. The composite structure of claim 4 , wherein the tool and the composite structure have a same or a similar coefficient of thermal expansion.

6. The composite structure of claim 3 , wherein the electrical contact is copper tape.

7. The composite structure of claim 4 , wherein the composite structure is insulated from the tool using an insulated material.

8. The composite structure of claim 2 , wherein the first portion is located near a first edge of the composite structure and the the second portion is located near a second edge of the composite structure, and wherein the portion of the composite structure includes at least a region between the first edge and the second edge.

9. The composite structure of claim 1 , wherein the temperature of the portion is measured via a thermocouple positioned at a surface of the composite structure.

10. The composite structure of claim 1 , wherein the composite structure is positioned electrically in series with a resistive load during the process such that the electric power source passes the electric current through the composite structure and the resistive load, wherein the resistive load comprises two or more resistors electrically connected to one another in parallel.

11. The composite structure of claim 1 , wherein the composite structure does not comprise a carbon nanotube material.

12. A composite structure comprising:
a composite laminate comprising a first material ply and a second material ply, wherein the composite structure is cured by a process comprising the steps of:
passing an electric current through the composite structure from a first portion of the composite structure to a second portion composite structure using an electric power source to increase a temperature of a portion of the composite structure to a predetermined temperature, wherein an electrical contact is positioned between the first material ply and the second material ply at each of the first portion and the second portion to improve conductivity across the composite structure; and
subjecting the composite structure to pressure using a vacuum while the electric current passes through the composite structure.

13. The composite structure of claim 12 , wherein the composite structure comprises an embeddable conductor layer between the first material ply and the second material ply.

14. The composite structure of claim 13 , wherein the embeddable conductor layer comprises a graphene material.

15. The composite structure of claim 13 , wherein the embeddable conductor layer comprises a carbon nanotube (CNT) material.

16. The composite structure of claim 15 , wherein the CNT material is vertically-aligned with the first material ply and the second material ply.

17. The composite structure of claim 15 , wherein the CNT material is aligned in-plane with the first material ply and the second material ply.

18. The composite structure of claim 15 , wherein the CNT material is arranged in a zig-zag pattern.

19. The composite structure of claim 12 , wherein the composite structure does not comprise a carbon nanotube material.

20. A composite structure comprising:
a composite laminate comprising a first material ply and a second material ply, wherein the composite structure is cured by a process comprising the steps of:
passing an electric current through the composite structure using an electric power source to increase a temperature of a portion of the composite structure to a predetermined temperature, wherein the composite structure does not comprise a carbon nanotube material; and
subjecting the composite structure to a vacuum pressure while the electric current passes through the composite structure.

21. The composite structure of claim 20 , wherein the electric power source is coupled to the composite structure via a first and a second electrical contact to improve conductivity across the composite structure, wherein each of the first electrical contact and the second electrical contact is positioned between the first material ply and the second material ply.

22. The composite structure of claim 21 , wherein each of the first and the second electrical contact is a copper tape.

23. The composite structure of claim 20 , wherein the composite structure is cured while the composite structure is freestanding.

24. The composite structure of claim 23 , wherein the composite structure is laid up using a tool having a coefficient of thermal expansion that is substantially similar to a coefficient of thermal expansion of the composite structure.

25. The composite structure of claim 1 , wherein the composite structure is positioned electrically in series with a resistive load such that the electric power source passes the electric current through the composite structure and the resistive load.

Assignees

• Aurora Flight Sciences Corp

Inventors

• Fetfatsidis Konstantine
• Reagan Daniel
• Tolmachov Denis
• Breingan Kyle
• Hemstreet Darlene

Classifications

• B32B2262/106

  Carbon fibres, e.g. graphite fibres · CPC title

• B32B2262/0269

  Aromatic polyamide fibres · CPC title

• H05B3/0004

  Devices wherein the heating current flows through the material to be heated (Circuit arrangements for heating by passing the current directly across the material to be heated H05B3/0023; granular, powdered or fluid material H05B3/60) · CPC title

• B32B2260/021

  Fibrous or filamentary layer · CPC title

• B32B2260/046

  Synthetic resin · CPC title