IP Library › Granted Patent US 11,649,845
Granted Patent B2
US 11,649,845 · App. 16/715,469 · Granted May 16, 2023

Mechanical fastener system for electromagnetic effect (EME) protection

Inventors: Darrin M. Hansen (Seattle, WA); Blake A. Simpson (Kent, WA); Richard B. Tanner (Seattle, WA); Peter K. Augusciak (Shoreline, WA)
Assignee: THE BOEING COMPANY
F16B33/06B64D45/02F16B5/02F16B2200/00
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Quick Facts
Patent No.
US 11,649,845
App. No.
16/715,469
Granted
May 16, 2023
Kind
B2
Abstract

A mechanical fastener system for EME protection, including at least one plated component, wherein the at least one plated component includes a base material, a bonding layer disposed over the base material, and a metal plating disposed over the bonding layer.

Claims (49)

1. A mechanical fastener system for EME protection, comprising:

at least one plated component,

wherein the at least one plated component comprises:

a base material comprising at least one of titanium, corrosion-resistant steel, Inconel, and alloys or combinations thereof,

a bonding layer comprising one or more of nickel, iron, copper, and alloys or combinations thereof disposed over the base material, and

a metal plating comprising at least one of indium, tin, zinc, bismuth, and alloys and combinations thereof disposed over the bonding layer, and

wherein there is substantially no protective oxide layer between the base material and the bonding layer.

2. The mechanical fastener system for EME protection of claim 1 , wherein the at least one plated component comprises one or more of:

a fastener comprising a head, a threaded portion, and a shank extending between said head and said threaded portion;

a nut configured to engage a threaded portion of a fastener;

a collar configured to engage a threaded portion of a fastener;

a washer configured to be disposed on a fastener between a threaded portion and a head of the fastener; and

a sleeve configured to engage a threaded portion of a fastener, wherein the sleeve is configured to deform when engaged by the fastener.

3. The mechanical fastener system for EME protection of claim 1 , further comprising one or more components,

wherein the one or more components comprise one or more of:

a fastener comprising a head, a threaded portion, and a shank extending between said head and said threaded portion;

a nut configured to engage a threaded portion of a fastener;

a collar configured to engage a threaded portion of a fastener;

a washer configured to be disposed on a fastener between a threaded portion and a head of a fastener; and

a sleeve configured to engage a threaded portion of a fastener, wherein the sleeve is configured to deform when engaged by the fastener.

4. A mechanical fastener system for EME protection, comprising:

at least one plated component,

wherein the at least one plated component comprises:

an etched base material,

a bonding layer disposed over the etched base material, and

a metal plating disposed over the bonding layer, and

wherein there is substantially no protective oxide layer between the etched base material and the bonding layer.

5. The mechanical fastener system for EME protection of claim 1 , wherein the base material for the plated component has a hydrogen content of about 0.0125 weight % (125 PPM) or lower.

6. The mechanical fastener system for EME protection of claim 1 , wherein the base material for the plated component comprises an etched base material layer.

7. The mechanical fastener system for EME protection of claim 4 , wherein the base material for the plated component comprises at least one of titanium, corrosion-resistant steel, Inconel, and alloys or combinations thereof.

8. The mechanical fastener system for EME protection of claim 4 , wherein the bonding layer comprises one or more of nickel, iron, copper, and alloys or combinations thereof.

9. The mechanical fastener system for EME protection of claim 1 , wherein the bonding layer has a thickness from about 0.01 mils to about 0.5 mils.

10. The mechanical fastener system for EME protection of claim 4 , wherein the metal plating comprises one or more lubricious and conductive metals.

11. The mechanical fastener system for EME protection of claim 4 , wherein the metal plating comprises at least one of indium, tin, zinc, bismuth, and alloys and combinations thereof.

12. The mechanical fastener system for EME protection of claim 1 , wherein the metal plating comprises indium.

13. The mechanical fastener system for EME protection of claim 1 , wherein the metal plating has a thickness from about 0.05 mils to about 1.0 mils.

14. The mechanical fastener system for EME protection of claim 10 , wherein a friction coefficient of the metal plating is equal to or lower than the friction coefficient of a soft metal.

15. The mechanical fastener system for EME protection of claim 10 , wherein a friction coefficient of the metal plating is equal to or lower than a friction coefficient of indium (In).

16. The mechanical fastener system for EME protection of claim 10 , wherein a conductivity of the metal plating is from about 2×10 5 S/m to about 6.3×10 7 S/m.

17. The mechanical fastener system for EME protection of claim 1 , wherein the metal plating is galvanically compatible with at least one of titanium, corrosion-resistant steel, Inconel, aluminum, and alloys and combinations thereof.

18. A joined structure with EME protection, comprising:

two or more substrates; and

at least one mechanical fastener system comprising at least one plated component, wherein the at least one plated component comprises an etched base material, a bonding layer disposed on the etched base material, and a metal plating disposed on the bonding layer,

wherein the at least one mechanical fastener system is used to join the two or more substrates,

wherein the two or more substrates comprise composite substrates, metal substrates, and combinations thereof, and

wherein there is substantially no protective oxide layer between the etched base material and the bonding layer.

19. The joined structure with EME protection of claim 18 , wherein a friction coefficient of the metal plating is equal to or lower than a friction coefficient of indium (In), and

wherein a conductivity of the metal plating is from about 2×10 5 S/m to about 6.3×10 7 S/m.

20. The joined structure with EME protection of claim 18 , wherein the etched base material comprises at least one of titanium and alloys thereof, and wherein the metal plating comprises indium.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 16, 2019
From: HANSEN, DARRIN M.; SIMPSON, BLAKE A.; TANNER, RICHARD B.; AUGUSCIAK, PETER K.
To: THE BOEING COMPANY
Reel/Frame 051294/0462 →
Continuity (1)
Related Publication 20210180636A1 · Jun 17, 2021