Modified shank fasteners for electromagnetic effect (EME) technology

Patent metadata

Field	Value
Publication number	US-9908637-B2
Application number	US-201414286612-A
Country	US
Kind code	B2
Filing date	May 23, 2014
Priority date	May 23, 2014
Publication date	Mar 6, 2018
Grant date	Mar 6, 2018

Abstract

A fastener system for composite structure providing electromagnetic energy protection has a shank with a threaded portion on a first end of the shank terminating in a lead-in portion. A head is present on a second end of the shank. The shank is adapted for intimate conductive contact with an inner surface of an interference fit hole.

First claim

What is claimed is:

1. A fastener system for composite structure comprising;
a shank having a roughened main body with peaks and valleys;
a lubricious coating on the main body said coating polished for exposure of the peaks
a threaded portion on a first end of the shank with a lead-in portion transitioning between the threaded portion and the main body; and,
a head on a second end of the shank;
wherein the shank is configured for intimate conductive contact with an inner surface of an interference fit hole in a composite with the lead-in portion transitionally engaging the main body with an inner surface of the hole, the peaks maintaining intimate conductive contact, the lubricious coating remaining present in the valleys for lubricious insertion of the main body into the interference fit hole.

2. The fastener system as defined in claim 1 wherein the lead-in portion is configured to expand the inner surface of the interference fit hole without damaging the composite.

3. The fastener system as defined in claim 2 wherein the shank is adapted to be in intimate conductive contact with the inner surface of the hole to conduct large current densities.

4. The fastener system as defined in claim 1 wherein the threaded portion and the lead in portion are coated in dry lubricant.

5. The fastener system as defined in claim 1 wherein the roughened main body is knurled.

6. The fastener system as defined in claim 1 wherein the lubricious coating is one of a phenolic resin base containing lubricating pigments, epoxy based coatings, and other solid film lubricants that are resin or ceramic based, with solid lubricant additives.

7. A method for EME protection of fasteners in composite structures comprising:
identifying a hole in a composite joint for installation of a fastener having a threaded portion on a first end of the shank terminating in a lead-in portion and a head on a second end of the shank;
establishing a fastener diameter for an interference fit in the hole;
forming a roughened surface on a main body of the shank of a fastener with peaks having the established diameter;
coating the fastener main body with a lubricious coating;
polishing the roughened surface to remove the lubricious coating from the peaks of the roughed surface but allowing the coating to remain in valleys said peaks adapted for an interference fit in the hole maintaining intimate conductive contact, the lubricious coating remaining present in the valleys for lubricious insertion into the hole;
inserting the fastener into the hole;
transitionally engaging the main body with an inner surface of the hole with a lead-in portion to provide the interference fit;
forming with the interference fit an intimate conductive contact between the shank and hole; and,
transferring electrical energy from the peaks to a surface of the hole during an EME event.

8. The method of claim 7 wherein the step of forming a roughened surface comprises knurling the main body of the shank.

9. The method of claim 7 wherein the step of coating the fastener main body with a lubricious coating comprises applying a dry aluminum pigmented coating.

10. The method as defined in claim 9 where in the aluminum pigmented coating comprises a phenolic resin containing aluminum flakes or particles.

11. The method of claim 7 wherein the step of coating the fastener main body with a lubricious coating comprises applying a coating selected from an epoxy based coating or solid film lubricant having a resin or ceramic base.

12. The method of claim 7 wherein the step of identifying a hole in a composite structure comprises identifying a hole in a composite structure in a production process for installation of a fastener having a threaded portion on a first end of the shank terminating in a lead-in portion and a head on a second end of the shank.

13. The method of claim 7 wherein the step of identifying a hole in a composite structure comprises identifying a hole in a composite structure in a maintenance process for installation of a fastener having a threaded portion on a first end of the shank terminating in a lead-in portion and a head on a second end of the shank.

Assignees

• Boeing Co

Inventors

• Whitlock Richard P
• Coronado Peter A
• Pacheco Agosto Omar J
• Ware Michael H E

Classifications

• F16B33/06 Primary

  Surface treatment of parts furnished with screw-thread, e.g. for preventing seizure {or fretting (corrosion preventing means F16B33/008; settable coatings for locking threaded members F16B39/225; deformable coatings for locking threaded members F16B39/34)} · CPC title

• B64D45/02 Primary

  Lightning protectors; Static dischargers · CPC title

• Y10T29/49886

  to roughen surface · CPC title

• F16B35/048

  Specially-shaped necks (F16B35/06 takes precedence) · CPC title

• F16B35/04

  with specially-shaped head or shaft in order to fix the bolt on or in an object (locking the bolt against turning in the object by the use of accessory parts F16B39/00) · CPC title