Thrust bearing seal for thin wing multi slice RGA

Patent metadata

Field	Value
Publication number	US-12006977-B2
Application number	US-202217592914-A
Country	US
Kind code	B2
Filing date	Feb 4, 2022
Priority date	Feb 8, 2021
Publication date	Jun 11, 2024
Grant date	Jun 11, 2024

Abstract

A thrust bearing seal for radially sealing a gap between a first component and a second component. The seal includes an external sealing cap that extends circumferentially around an outer circumferential surface of at least a section of said first component and a projection that extends radially inwardly from said external sealing cap and into said gap.

First claim

The invention claimed is:

1. A thrust bearing seal for radially sealing a gap between a first component and a second component, the seal comprising:
an external sealing cap that extends circumferentially around an outer circumferential surface of at least a section of said first component; and
a projection that extends radially inwardly from said external sealing cap and into said gap, wherein said projection further comprises means configured to axially seal said second component and said gap;
wherein said means are configured to axially seal to provide an axial force against the second, or fixed component in use and also comprises:
an axially extending circumferential lip that extends from the radially innermost point of the inwardly protruding section.

2. The seal of claim 1 , wherein said external sealing cap also extends circumferentially around an outer surface of at least a section of said second component.

3. The seal of claim 2 , wherein:
said seal has a T-shaped cross section having a post and an upper part; and
said projection comprises the post of the T shape and said external sealing cap is ring-shaped and comprises the upper part of the T shape.

4. The seal of claim 2 , wherein said external sealing cap is configured so as to provide a radially inward force against the components, and a circumferential sealing contact with said first and second components.

5. The seal of any of claim 4 , claim wherein said external sealing cap has a non-uniform cross-sectional thickness.

6. The seal of claim 5 , wherein the non-uniform cross-sectional thickness of the external sealing cap is reduced at a junction either side of the inwardly extending section of the external sealing cap and the projection.

7. The seal of claim 1 , further comprising:
a clamp spring provided on the external surface of the external sealing cap of the thrust bearing seal.

8. The seal of claim 1 , wherein said circumferential lip is ring shaped and configured to provide a circumferential and axial force against the second component.

9. The seal of claim 1 , wherein at a junction between the external sealing cap and the inwardly extending projection, on an internal surface of the cap, the cross section thickness of the cap has a reduced cross sectional thickness in comparison to an adjacent section of the cap that extends over the first component.

10. The seal of claim 1 , wherein a cross sectional thickness at the junction between the inwardly extending projection and the lip is reduced in thickness in comparison to the adjacent section of the projection or the lip.

11. The seal of claim 1 , wherein the first component and the second component are components of a rotary geared actuator.

12. The seal of claim 1 , wherein the first component is a rotating component and said second component is a fixed component.

Assignees

• Goodrich Actuation Systems Ltd

Inventors

• Darby Jonathan

Classifications

• F16J15/3236

  with at least one lip for each surface, e.g. U-cup packings · CPC title

• F16J15/3216

  supported in a direction parallel to the surfaces · CPC title

• F16C17/04

  for axial load only · CPC title

• B64C13/28

  mechanical · CPC title

• F16C2361/61

  Toothed gear systems, e.g. support of pinion shafts · CPC title