System for isolating electrical current in a bearing for use in an aircraft structure

Patent metadata

Field	Value
Publication number	US-9482269-B2
Application number	US-201514857055-A
Country	US
Kind code	B2
Filing date	Sep 17, 2015
Priority date	Sep 17, 2014
Publication date	Nov 1, 2016
Grant date	Nov 1, 2016

Abstract

A system for isolating electrical current in an aircraft structure includes a first structure a bearing having an outer race and an inner race and a liner disposed therebetween, the outer race having a second structure coupled thereto. A dielectric seal is secured to the outer race and engages the inner race. A conditionally non-conductive gas occupies a sealed chamber that defines a gap between the inner race and the outer race. The gap has a predetermined magnitude sufficient to prevent electrical arcing or current leakage between the inner race and the outer race at a first voltage less than that voltage resulting from a lightning strike; and/or to conduct an electrical current between the inner race and the outer race at a second voltage greater than or equal to the voltage resulting from the lightning strike.

First claim

What is claimed is:

1. A system for isolating electrical current in an aircraft structure, the system comprising:
a first structure;
a bearing comprising:
an outer race defining an outer race inner surface and an outer race side surface;
an inner race disposed partially in the outer race and coupled to the first structure, the inner race defining an inner race outer surface; and
a liner disposed between the outer race inner surface and the inner race outer surface;

a second structure coupled to the outer race;
a dielectric seal secured to the outer race side surface and sealingly and slidingly engaging the inner race outer surface;
a sealed chamber defined by the dielectric seal, the outer race inner surface, the inner race outer surface and an edge of the liner;
a conditionally non-conductive gas for conditionally electrically isolating the first structure from the second structure, the conditionally non-conductive gas fluidly occupying the sealed chamber; and
the sealed chamber defines a minimum gap between the inner race outer surface and the outer race inner surface, the gap has at least one of:
a predetermined magnitude sufficient to prevent electrical arcing or current leakage between the inner race outer surface and the outer race inner surface at a first voltage, the first voltage being less than a voltage resulting from a lightning strike; and
a predetermined magnitude sufficient to conduct an electrical current between the inner race outer surface and the outer race inner surface at a second voltage, the second voltage being at least as great as the voltage resulting from the lightning strike.

2. The system of claim 1 , wherein the conditionally non-conductive gas has an electrical resistance, at the gap, of a magnitude sufficient to cause the electrical current to preferentially flow through the gap, instead of through the liner.

3. The system of claim 1 , wherein the conditionally nonconductive gas is air.

4. The system of claim 1 , wherein the conditionally non-conductive gas is operable to electrically isolate the first structure from the second structure if the first voltage is less than a threshold voltage, and electrically coupling the first structure to the second structure if the second voltage is greater than the threshold voltage.

5. The system of claim 1 , wherein the bearing is one of a spherical bearing, a bushing, and a journal bearing.

6. The system of claim 1 , wherein the dielectric seal comprises at least one of polytetrafluoroethylene, plastic and rubber.

7. The system of claim 1 , wherein the liner is a continuous form.

8. The system of claim 1 , wherein the second voltage is at least about 350 volts.

9. The system of claim 1 , wherein the liner is configured to limit electrical current leakage from the inner race outer surface and the outer race inner surface at the second voltage.

10. The system of claim 1 , wherein the liner is configured to prevent electrical arcing between the inner race outer surface and the outer race inner surface at the second voltage.

Assignees

• Roller Bearing Co America Inc

Inventors

• Fruin John W
• Anderson Ben
• Simpson Maura
• Henn Andrew
• Bryant Kevin

Classifications

• F16C33/201

  Composition of the plastic · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16C23/045

  for radial load mainly, e.g. radial spherical plain bearings · CPC title

• F16C17/24 Primary

  with devices affected by abnormal or undesired positions, e.g. for preventing overheating, for safety · CPC title

• F16C23/043

  with spherical surfaces, e.g. spherical plain bearings · CPC title