Screw seal and lubrication

Patent metadata

Field	Value
Publication number	US-10895309-B2
Application number	US-201816059497-A
Country	US
Kind code	B2
Filing date	Aug 9, 2018
Priority date	Aug 25, 2017
Publication date	Jan 19, 2021
Grant date	Jan 19, 2021

Abstract

Disclosed herein is a screw assembly comprising an internal re-circulating path for re-circulating lubricant fluid between a threaded screw shaft and seals provided at the ends of the screw assembly via internal chambers provided within the seals and passages formed within the nut. Also disclosed are seals for use within such assemblies.

First claim

The invention claimed is:

1. A screw assembly comprising:
a screw shaft having a helical thread profile; and
a nut for mounting around said screw shaft;
the screw assembly further comprising a first seal and a second seal, wherein each of said first seal and said second seal independently comprises a seal, the seal comprising:
a seal body having an inner surface for mounting onto and sealing against a screw shaft;
an internal chamber formed within said seal body, wherein one or more openings are provided on said inner surface to allow lubricant material to transfer between said inner surface and said internal chamber; and one or more external ports provided on a radial surface and/or an outer surface of said seal body for transferring lubricant material into or out of said internal chamber of said seal body;

wherein respective external ports ( 27 A, 27 B) of said first and second seals ( 26 A, 26 B) are aligned with respective passages extending through said screw assembly to provide a re-circulating path for re-circulating lubricant material within said screw assembly.

2. The screw assembly of claim 1 , wherein said passages are formed within said nut such that said re-circulating path extends from the first seal ( 26 A) through the passage formed within the nut to the second seal.

3. The screw assembly of claim 1 , wherein said first seal ( 26 A) is disposed at a first end of said screw assembly and wherein said second seal ( 26 B) is disposed at a second, opposite end of said screw assembly.

4. The screw assembly of claim 1 , wherein a rotation of said screw shaft relative to the first and second seals in a clockwise direction causes lubricant material to flow around said re-circulating path in a first direction and wherein rotation of said screw shaft relative to the first and second seals in an anti-clockwise direction causes lubricant material to flow around said re-circulating path in a second, opposite direction.

5. The screw assembly of claim 1 , wherein said screw assembly is a ballscrew assembly comprising a plurality of ball bearings received within the thread profile of said screw shaft and wherein said nut radially confines said ball bearings within the ballscrew assembly.

6. An aircraft comprising: the screw assembly of claim 1 .

7. An aircraft control system comprising: the screw assembly of claim 1 .

Assignees

• Goodrich Actuation Systems Ltd

Inventors

• Holding James
• Hawksworth Andrew

Classifications

• F16J15/324

  Arrangements for lubrication or cooling of the sealing itself · CPC title

• F16J15/32

  with elastic sealings, e.g. O-rings · CPC title

• F16H57/0497

  Screw mechanisms · CPC title

• F16H25/2418 Primary

  Screw seals, wipers, scrapers or the like · CPC title

• F16H25/2204

  with balls · CPC title