Fastener using lubricated interference fit

Patent metadata

Field	Value
Publication number	US-11560910-B2
Application number	US-202016742274-A
Country	US
Kind code	B2
Filing date	Jan 14, 2020
Priority date	Sep 30, 2014
Publication date	Jan 24, 2023
Grant date	Jan 24, 2023

Abstract

The invention relates to a method for installing metallic fastener ( 10; 40 ) for the interference fit assembly of at least two structural elements ( 20, 22 ) comprising a through hole, the fastener comprising an enlarged head ( 12; 42 ), a shaft ( 14; 44 ) having an external diameter before installation that is greater than an internal diameter of the hole, said shaft comprising a conductive surface ( 26; 56 ). Before installation, at least the conductive surface ( 26; 56 ) is coated with a lubricating layer ( 30 ), which comprises a mixture of at least one polyolefin and one polytetrafluoroethylene, for example, having sufficient adherence to prevent its abrasion by manual manipulation of the fastener and being weak enough to be at least partly stripped from the conductive surface during the interference fit assembly of the fastener. The invention is applicable to the assembly of aircraft structures.

First claim

The invention claimed is:

1. A method for installing a metallic fastener a hole passing through at least two structural elements, the fastener comprising an enlarged head and a shaft having an external diameter D 1 before installation that is greater than an internal diameter D 3 of the hole, said shaft comprising a conductive surface,
wherein at least the conductive surface includes a coating with a lubricating layer comprising a mixture of at least one polyolefin and one polytetrafluoroethylene, and wherein during the installation, inserting the fastener into the hole wherein the lubricating layer has a composition determined so as to have sufficient adherence to prevent its abrasion by manual manipulation of the fastener and to be weak enough to be at least partly stripped from the conductive surface during the interference fit insertion of the fastener and comprises at least 80% by weight of polyolefin and polytetrafluoroethylene, and during a step of inserting the shaft of the fastener into the structure through an interference fit, the lubricating layer is partly stripped from the shaft of the screw.

2. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the lubricating layer is, before installation, between 8.3 μm and 23.5 μm thick.

3. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the lubricating layer is, after installation, between 0.9 μm and 2.1 μm thick.

4. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface comprises a sulfuric anodization layer that is less than 1 μm thick.

5. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface is a metal having undergone a passivation operation.

6. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface is an aluminum layer deposited in a vacuum.

7. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface comprises the entire external surface of the shaft.

8. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the lubricating layer further coats a threaded portion of the fastener.

9. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the fastener further comprises a traction tail and a shear groove designed to break under a certain tensile stress.

10. The method according to claim 1 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface comprises only one portion of the external surface of the shaft.

11. The method according to claim 10 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface comprises an annular portion of the shaft of the fastener.

12. The method according to claim 10 , wherein inserting the fastener includes inserting the fastener wherein the conductive surface comprises an axial portion of the shaft of the fastener.

Assignees

• Lisi Aerospace

Inventors

• Bourges Laurent
• Stephan Johan
• Van Daele Christophe

Classifications

• F16B33/008

  Corrosion preventing means · CPC title

• C23C26/00

  Coating not provided for in groups C23C2/00 - C23C24/00 · CPC title

• F16B2001/0064

  Mechanical Engineering · mapped topic

• C10M2201/105

  Silica · CPC title

• B05D3/0493

  using vacuum · CPC title