Plain journal bearing

Patent metadata

Field	Value
Publication number	US-9321522-B2
Application number	US-201213644333-A
Country	US
Kind code	B2
Filing date	Oct 4, 2012
Priority date	Oct 27, 2011
Publication date	Apr 26, 2016
Grant date	Apr 26, 2016

Abstract

A plain journal bearing couples first and second components. A pin passes through the components. A clamping bush surrounds the pin. A clamping member is mounted on the pin and provides a clamping force to urge the clamping bush into clamping engagement with the first component. During normal operation, when the components rotate relative to each other, the second component and the clamping bush rotate relative to each other about a primary slip path, and the clamping bush remains in clamping engagement with the first component. During degraded operation, when the components rotate relative to each other and the coefficient of friction of the primary slip path has increased to overcome the clamping force, the pin and the clamping bush or the pin and the first component rotate relative to each other about a subsidiary slip path.

First claim

The invention claimed is:

1. A plain journal bearing coupling a first component to a second component, the bearing comprising:
a pin which passes through the first component and the second component;
a clamping bush which surrounds the pin and has a cylindrical inner surface, a cylindrical outer surface, and an end face; and
a clamping member which is mounted on the pin and provides a clamping force between the end face of the clamping bush and the first component,
wherein the bearing has a primary slip path between the outer surface of the clamping bush and the second component, the primary slip path having an initial coefficient of friction sufficiently low that, when the first and second component rotate relative to each other, the second component and the clamping bush rotate relative to each other about the primary slip path and the clamping bush remains in clamping engagement with the first component; and
wherein the pin has a cylindrical outer surface which provides a subsidiary slip path which is arranged to operate when the coefficient of friction of the primary slip path has been sufficiently increased due to use that a friction force between the clamping bush and the second component overcomes the clamping force, whereby when the first and second component rotate relative to each other, the pin and the clamping bush rotate relative to each other about the subsidiary slip path.

2. The bearing of claim 1 wherein the cylindrical outer surface of the in provides:
a first subsidiary slip path which is arranged to operate when the coefficient of friction of the primary slip path has been sufficiently increased due to use that a friction force between the clamping bush and the second component exceeds the clamping force, whereby when the first and second component rotate relative to each other, the pin and the clamping bush can rotate relative to each other about the first subsidiary slip path; and
a second subsidiary slip path which is arranged to operate when the coefficient of friction of the primary slip path has been sufficiently increased due to use that a friction force between the clamping bush and the second component overcomes the clamping force, whereby when the first and second component rotate relative to each other, the pin and the first component can rotate relative to each other about the second subsidiary slip path.

3. The bearing of claim 2 wherein the first subsidiary slip path has a lower coefficient of friction than the second subsidiary slip path.

4. The bearing of claim 1 wherein the first and/or second subsidiary slip path comprises a layer of low coefficient of friction material.

5. The bearing of claim 4 wherein the layer of low coefficient of friction material comprises a coating of low friction material which is adhered to an inner diameter of the clamping pin or an outer diameter of the pin.

6. The bearing of claim 1 wherein a layer of low coefficient of friction material is provided between the clamping bush and the first component.

7. The bearing of claim 6 wherein the layer of low coefficient of friction material comprises a coating of low friction material which is adhered to the end face of the clamping bush.

8. The bearing of claim 1 wherein a layer of low coefficient of friction material is provided between the clamping bush and the clamping member.

9. The bearing of claim 1 wherein the bearing is installed on an aircraft.

10. The bearing of claim 1 wherein the first component is a flight control element and the second component is a main wing element.

11. The bearing of claim 1 wherein the clamping member comprises a threaded nut which is screwed onto the pin.

12. A plain journal bearing coupling a first component to a second component, the bearing comprising:
a pin which passes through the first component and the second component;
a clamping bush which surrounds the pin and has a cylindrical inner surface, a cylindrical outer surface, and an end face; and
a clamping member which is mounted on the pin and provides a clamping force between the end face of the clamping bush and the first component,
wherein the bearing has a primary slip path between the outer surface of the clamping bush and the second component, the primary slip path having an initial coefficient of friction sufficiently low that, when the first and second component rotate relative to each other, the second component and the clamping bush rotate relative to each other about the primary slip path and the clamping bush remains in clamping engagement with the first component; and
wherein the pin has a cylindrical outer surface which provides a subsidiary slip path which is arranged to operate when the coefficient of friction of the primary slip path has been sufficiently increased due to use that a friction force between the clamping bush and the second component overcomes the clamping force, whereby when the first and second component rotate relative to each other, the pin and the first component rotate relative to each other about the subsidiary slip path.

13. An installation on an aircraft, the installation comprising a main wing element; a flight control element; and a bearing according to claim 1 coupling the main wing element to the flight control element.

Assignees

• Airbus Operations Ltd

Inventors

• Blades Paul

Classifications

• Y10T403/32909

  Threaded pin end · CPC title

• F16C11/02

  Trunnions; Crank-pins (fastening crank-pins to webs, crank-pins integral with cranks F16C3/06, F16C3/22) · CPC title

• B64C9/02 Primary

  Mounting or supporting thereof · CPC title

• Y10T29/49948

  Multipart cooperating fastener [e.g., bolt and nut] · CPC title

• Y02T50/44

  Cross-Sectional Technologies · mapped topic