Bearing arrangement and method

Patent metadata

Field	Value
Publication number	US-9470262-B2
Application number	US-201514631245-A
Country	US
Kind code	B2
Filing date	Feb 25, 2015
Priority date	Mar 19, 2014
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

A bearing arrangement comprises: first and second thrust bearings, each including an inner race which is disposed on a shaft and an outer race which is supported by at least one resilient element. Applying a shaft thrust load elastically deforms the resilient elements so as to axially displace the respective outer races in order that the thrust load is shared between the first and second thrust bearings.

First claim

The invention claimed is:

1. A bearing arrangement comprising:
a first thrust bearing and a second thrust bearing, each of the first thrust bearing and the second thrust bearing including:
an inner race disposed on a shaft; and
an outer race supported by at least one resilient element, wherein:

applying a shaft thrust load elastically deforms the at least one resilient element of the respective outer races of the first thrust bearing and the second thrust bearing so as to axially displace the respective outer races of the first thrust bearing and the second thrust bearing such that the shaft thrust load is shared between the first thrust bearing and the second thrust bearing;
when in an undeformed condition, each of the resilient elements is within a projected axial length of the respective first thrust bearing and second thrust bearing; and
when in an elastically deformed condition, each of the resilient elements extends beyond the projected axial length of the respective first thrust bearing and second thrust bearing.

2. The bearing arrangement according to claim 1 , wherein the resilient elements are elastically deformed such that the thrust load is substantially equally shared between the first thrust bearing and the second thrust bearing.

3. The bearing arrangement according to claim 1 , wherein:
the outer race of each of the first thrust bearing and the second thrust bearing is supported by two resilient elements; or
the outer race of each of the first thrust bearing and the second thrust bearing is supported by four resilient elements.

4. The bearing arrangement according to claim 3 , wherein the four resilient elements are arranged in pairs.

5. The bearing arrangement according to claim 1 , wherein:
when in the undeformed condition, each of the resilient elements extends substantially perpendicular to an axial direction; or
when in the undeformed condition, each of the resilient elements is inclined relative to an imaginary line which extends perpendicular to the axial direction.

6. The bearing arrangement according to claim 1 , wherein the resilient elements include diaphragms.

7. The bearing arrangement according to claim 6 , wherein the diaphragms are curved.

8. The bearing arrangement according to claim 1 , wherein the first thrust bearing and the second thrust bearing are axially spaced on the shaft.

9. The bearing arrangement according to claim 8 , further comprising a spacer element disposed between the inner races of the respective first thrust bearing and second thrust bearing to define an axial distance between the first thrust bearing and the second thrust bearing.

10. The bearing arrangement according to claim 1 , further comprising at least one measurement device configured to measure axial displacements of the outer races of the respective first thrust bearing and second thrust bearing.

11. The bearing arrangement according to claim 1 , wherein the outer races of the respective first thrust bearing and second thrust bearing are supported by the respective resilient elements on a bearing housing of a gas turbine engine.

12. A gas turbine engine, comprising the bearing arrangement according to claim 1 .

13. A bearing arrangement comprising:
a first thrust bearing and a second thrust bearing, each of the first thrust bearing and the second thrust bearing including:
an inner race on a shaft; and
an outer race supported by at least one resilient element, wherein:

applying a shaft thrust load axially displaces the respective outer races of the first thrust bearing and the second thrust bearing against resistance from the respective resilient elements of the first thrust bearing and the second thrust bearing so that the shaft thrust load is shared between the first thrust bearing and the second thrust bearing;
when in an undeformed condition, each of the resilient elements is within a projected axial length of the respective first thrust bearing and second thrust bearing; and
when in an elastically deformed condition, each of the resilient elements extends beyond the projected axial length of the respective first thrust bearing and second thrust bearing.

Assignees

• Rolls Royce Plc

Inventors

• Gallimore Stephen
• Fletcher Paul
• Webster John Richard
• Maguire Alan Robert

Classifications

• F16C2360/23

  Gas turbine engines · CPC title

• F16C19/16

  with a single row of balls · CPC title

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• F16C41/02

  Arrangements for equalising the load on a plurality of bearings or their elements · CPC title