Enhancing z-conductivity in carbon fiber reinforced plastic composite layups

Patent metadata

Field	Value
Publication number	US-10472473-B2
Application number	US-201514721880-A
Country	US
Kind code	B2
Filing date	May 26, 2015
Priority date	May 26, 2015
Publication date	Nov 12, 2019
Grant date	Nov 12, 2019

Abstract

Carbon fiber reinforced plastic (“CFRP”) composite layups and processes for manufacturing CFRP composite layups that integrate z-conductivity features directly into CFRP composite layups during the manufacturing processes for lightning protection, more particularly, inherent edge glow protection from lightning direct effects, and electrical current flow path control. CFRP composite layups are configured during the manufacturing processes to provide inter-ply electrical connections between composite plies of the CFRP composite layups, therefore avoiding the need for add-on protection features that result in significant cost and weight penalties.

First claim

The invention claimed is:

1. A CFRP composite layup comprising:
a plurality of composite plies, each having a conductive carbon fiber reinforcement material surrounded by a non-conductive matrix material and a cut edge where ends of the conductive carbon fiber reinforcement material are exposed,
two or more of the composite plies having an out-of-plane distortion where the conductive carbon fiber reinforcement material in each of the two or more composite plies is closer together to form inter-ply electrical connections about 1 inch or less from the cut edge where a thickness of the non-conductive matrix material is reduced and at least a portion of the conductive carbon fiber reinforcement material in each of the composite plies is electrically connected to at least a portion of the conductive carbon fiber reinforcement material in an adjacent ply of the CFRP composite layup such that the carbon fiber reinforcement material in a lower ply at a lower surface of the CFRP composite layup is electrically connected to the carbon fiber reinforcement material in an upper ply at an upper surface of the CFRP composite layup through the carbon fiber reinforcement material in one or more inner plies between the upper ply and the lower ply.

2. The CFRP composite layup of claim 1 , further comprising one or more layered forming tools consisting of cured carbon fiber composite layups of specific dimensions smaller than dimensions of the CFRP composite layup embedded between at least two of the composite plies, the out-of-plane distortion formed at an edge of the forming tools.

3. The CFRP composite layup of claim 2 , wherein a first of the one or more layered forming tools is embedded between the upper ply of the CFRP composite layup and a first ply of the inner plies at a first position along a length of the CFRP composite layup to form a first out-of-plane distortion, and a second of the one or more layered forming tools is embedded between a second ply and a third ply of the inner plies at a second position along the length of the CFRP composite layup to form a second out-of-plane distortion staggered in a lengthwise direction from the first out-of-plane distortion.

4. The CFRP composite layup of claim 1 , further comprising an electrically conductive material penetrating through an entire thickness of the CFRP composite layup in one or more rows positioned about 1 inch or less from the cut edge to electrically short the carbon fiber reinforcement material in each of the composite plies to form the inter-ply electrical connections.

5. The CFRP composite layup of claim 4 , wherein the electrically conductive material has a conductivity of at least 10 4 Siemens/meter.

6. The CFRP composite layup of claim 4 , wherein the one or more rows of the electrically conductive material are staggered at different distances from the cut edge.

7. A CFRP composite layup comprising:
a plurality of composite plies, each having a conductive carbon fiber reinforcement material surrounded by a non-conductive matrix material and a cut edge where ends of the conductive carbon fiber reinforcement material are exposed; and
a crimp through the plurality of composite plies that pushes the conductive carbon fiber reinforcement material in each of the composite plies together to form inter-ply electrical connections about 1 inch or less from the cut edge where a thickness of the non-conductive matrix material is reduced and at least a portion of the conductive carbon fiber reinforcement material in each of the composite plies is electrically connected to at least a portion of the conductive carbon fiber reinforcement material in an adjacent ply of the CFRP composite layup such that the carbon fiber reinforcement material in a lower ply at a lower surface of the CFRP composite layup is electrically connected to the carbon fiber reinforcement material in an upper ply at an upper surface of the CFRP composite layup through the carbon fiber reinforcement material in one or more inner plies between the upper ply and the lower ply.

8. The CFRP composite layup of claim 7 , wherein the crimp extends substantially parallel to the cut edge and across a width of the composite plies.

9. The CFRP composite layup of claim 7 , wherein the conductive carbon fiber reinforcement material in each of the composite plies are pushed together to within a distance of 10 micron or less.

10. The CFRP composite layup of claim 7 , wherein the crimp is a depressed area having a width of about 1 inch or less.

11. A CFRP composite layup comprising:
a plurality of composite plies, each having a conductive carbon fiber reinforcement material surrounded by a non-conductive matrix material and a cut edge where ends of the conductive carbon fiber reinforcement material are exposed, and
two or more of the composite plies having two or more out-of-plane distortions where the conductive carbon fiber reinforcement material in each of the two or more composite plies is closer together to form inter-ply electrical connections positioned at a plurality of locations throughout a length of the CFRP composite layup where a thickness of the non-conductive matrix material is reduced and at least a portion of the conductive carbon fiber reinforcement material in each of the composite plies is electrically connected to at least a portion of the conductive carbon fiber reinforcement material in an adjacent ply of the CFRP composite layup such that the carbon fiber reinforcement material in a lower ply at a lower surface of the CFRP composite layup is electrically connected to the carbon fiber reinforcement material in an upper ply at an upper surface of the CFRP composite layup through the carbon fiber reinforcement material in one or more inner plies between the upper ply and the lower ply.

12. The CFRP composite layup of claim 11 , further comprising one or more layered forming tools of specific dimensions smaller than dimensions of the CFRP composite layup embedded between at least two of the composite plies, the out-of-plane distortion formed at an edge of the forming tools.

13. The CFRP composite layup of claim 12 , wherein a first of the one or more layered forming tools is embedded between the upper ply of the CFRP composite layup and a first ply of the inner plies at a first position along a length of the CFRP composite layup to form a first out-of-plane distortion, and a second of the one or more layered forming tools is embedded between a second ply and a third ply of the inner plies at a second position along the length of the CFRP composite layup to form a second out-of-plane distortion staggered in a lengthwise direction from the first out-of-plane distortion.

14. The CFRP composite layup of claim 11 , further comprising a crimp through the plurality of composite plies that pushes and electrically shorts the conductive carbon fiber reinforcement material in each of the composite plies together to form the inter-ply electrical connections.

15. The CFRP composite layup of claim 14 , wherein the conductive carbon fiber reinforcement material in each of the composite plies are pushed together to within a distance of 10 micron or less.

16. The CFRP composite layup of claim 11 , further comprising an electrically conductive material penetrating through an entire thickness of the CFRP composite layup in one or more rows to electrically short the carbon fiber reinforcement material in each of the composite plies to form the inter-ply electrical connections.

17. The CFRP composite layup of claim 16 , wherein the electrically conductive material has a conductivity of at least

Assignees

• Boeing Co

Inventors

• Le Quynhgiao
• Greegor Robert B
• Whiting Brent Arthur

Classifications

• B29C70/025

  with particular filler · CPC title

• B29C70/882

  partly or totally electrically conductive, e.g. for EMI shielding (conductive floors or floor coverings H05F3/025; EMI shielding in general H05K9/00) · CPC title

• B29C70/545

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

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B32B5/10

  characterised by a fibrous {or filamentary} layer reinforced with filaments · CPC title