Conductive fastening system and method for improved EME performance

Patent metadata

Field	Value
Publication number	US-11137014-B2
Application number	US-201916242115-A
Country	US
Kind code	B2
Filing date	Jan 8, 2019
Priority date	Jan 8, 2019
Publication date	Oct 5, 2021
Grant date	Oct 5, 2021

Abstract

A conductive fastening system, a fastened assembly, and a method of fastening an assembly composed of layers of carbon fiber reinforced plastic (“CFRP”) and/or metallic material includes fasteners with an electrically conductive coating and electrically conductive gap filler materials between the fasteners and sidewalls of holes formed through the layers of the assembly. The sidewalls of the holes are coated with the electrically conductive gap filler material by abrading, injection or spraying. The fasteners with the electrically conductive coating are inserted through the holes. The conductive coating on the fasteners and electrically conductive gap filler material work together to enhance electrical conductivity between the fastener and assembly. The conductive coating also acts as a lubricant to reduce the amount of force required to insert the fastener into the hole thereby reducing damage to the assembly.

First claim

The invention claimed is:

1. A fastening system for an assembly comprising a first structural element made of a carbon fiber reinforced plastic (CFRP) having a first hole and a second structural element having a second hole aligned with the first hole of the first structural element, the fastening system comprising:
a fastener comprising a head, a mating portion, and a shank extending between the head and the mating portion, at least the mating portion and the shank insertable into the first hole and the second hole;
an electrically conductive coating formed on the shank of the fastener and having a uniform thickness of about 0.0001 inch to about 0.0006 inch; and
an electrically conductive gap filler applied to a sidewall of the first hole in the first structural element, the electrically conductive gap filler comprising a low melting alloy (LMA) made from one or more metals selected from the group consisting of bismuth, indium, tin, nickel, zinc, or combination thereof, and having particles that are deposited into crevices in the sidewall.

2. The fastening system of claim 1 , wherein the electrically conductive coating is made from one or more conductive metals selected from the group consisting of tin, zinc, indium, bismuth, combinations thereof, or alloys thereof.

3. The fastening system of claim 2 , further comprising a lubricating coating formed over the electrically conductive coating having a thickness of less than about 0.0002 inch, the lubricating coating positioned between the electrically conductive coating and the electrically conductive gap filler.

4. The fastening system of claim 1 , wherein the LMA has a first melting temperature lower than a second melting temperature of a matrix material of the CFRP.

5. The fastening system of claim 4 , wherein the first melting temperature of the LMA is in a range of about 140° F. to 400° F.

6. The fastening system of claim 1 , wherein the sidewall of the first hole has an irregular surface, and the electrically conductive gap filler forms a flattened surface over the irregular surface that decreases a diameter of the first hole by less than 0.0005 inch.

7. The fastening system of claim 1 , wherein the electrically conductive coating is a tin-zinc-bismuth alloy.

8. The fastening system of claim 1 , wherein the electrically conductive coating is a tin-bismuth alloy.

9. An assembly comprising:
a first structural element made of a carbon fiber reinforced plastic (CFRP) having a first hole;
a second structural element having a second hole aligned with the first hole of the first structural element;
a fastener comprising a head, a mating portion, and a shank extending between the head and the mating portion, the shank occupying at least respective portions of the first hole in the first structural element and the second hole in the second structural element, and the mating portion extending beyond the second structural element;
an electrically conductive coating formed on the shank of the fastener and having a uniform thickness of about 0.0001 inch to about 0.0006 inch; and
an electrically conductive gap filler positioned between the shank of the fastener and a sidewall of the first hole in the first structural element, the electrically conductive gap filler comprising a low melting alloy (LMA) made from one or more metals selected from the group consisting of bismuth, indium, tin, nickel, zinc, or combinations thereof, and having particles that are deposited into crevices in the sidewall.

10. The assembly of claim 9 , wherein the electrically conductive coating is made from one or more electrically conductive metals selected from the group consisting of tin, zinc, indium, bismuth combinations thereof, or alloys thereof.

11. The assembly of claim 10 , further comprising a lubricating coating formed over the electrically conductive coating having a thickness of less than about 0.0002 inch, the lubricating coating positioned between the electrically conductive coating and the electrically conductive gap filler.

12. The assembly of claim 9 , wherein the electrically conductive gap filler has a first melting temperature in a range of about 140° F. to about 400° F.

13. The assembly of claim 10 , wherein the sidewall of the first hole has an irregular surface, and the electrically conductive gap filler forms a flattened surface over the irregular surface that decreases a diameter of the first hole by less than 0.0005 inch.

14. The fastening system of claim 9 , wherein the electrically conductive coating is a tin-zinc-bismuth alloy.

15. The fastening system of claim 9 , wherein the electrically conductive coating is a tin-bismuth alloy.

16. The fastening system of claim 9 , wherein the LMA has a first melting temperature lower than a second melting temperature of a matrix material of the CFRP.

17. A method for fastening a first structural element made of a carbon fiber reinforced plastic (CFRP) having a first hole and a second structural element having a second hole aligned with the first hole, the method comprising the steps of:
applying an electrically conductive coating to a thickness of about 0.0001 inch to about 0.0006 inch on a shank of a fastener, the shank being positioned between a head and a mating portion of the fastener;
mechanically abrading an electrically conductive gap filler comprising a low melting alloy made from one or more metals selected from the group consisting of bismuth, indium, tin, nickel, zinc, or combinations thereof against a sidewall of the first hole in the first structural element to cause particles of the electricity conductive gap filler to be abraded and deposited into crevices in the sidewall;
inserting at least the mating portion and the shank of the fastener into the first hole of the first structural element and the second hole of the second structural element such that the shank occupies at least respective portions of the first hole and the second hole and the mating portion extends beyond the second structural element.

18. The method of claim 17 , wherein the electrically conductive gap filler is applied to flatten jagged edges in a surface of the sidewall of the first hole to create a soft, lubricious interface for installation of the fastener that decreases a diameter of the first hole by less than 0.0005 inch.

19. The method of claim 18 , wherein the electrically conductive gap filler is mechanically abraded onto the surface of the sidewall of the first hole at room temperature.

20. The method of claim 17 , further comprising concurrently measuring an effective resistance of the electrically conductive gap filler and carbon fibers in the CFRP as the electrically conductive gap filler is applied on the sidewall of the first hole and ceasing application of the electrically conductive gap filler when a specified effective resistance is achieved.

Assignees

• Boeing Co

Inventors

• Hansen Darrin M
• Simpson Blake A
• Khosravani Shahriar

Classifications

• B29L2031/7172

  Fuel tanks, jerry cans · CPC title

• B29L2031/3085

  Wings · CPC title

• B29L2031/3082

  Fuselages · CPC title

• B29L2031/3076

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

• B29C66/73141

  Electrical conductivity · CPC title