Bearing structure

Patent metadata

Field	Value
Publication number	US-9829037-B2
Application number	US-201514961124-A
Country	US
Kind code	B2
Filing date	Dec 7, 2015
Priority date	Dec 9, 2014
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

Load sharing stacked bearing structure including first bearing having a first inner race, first outer race and first set of roller elements housed between first inner race and first outer race and a second bearing having a second inner race, second outer race and second set of roller elements housed between second inner race and the second outer race. A housing surrounds the first and second bearings. First compliant element is provided with the first compliant element connected between the housing and the first outer race. The first compliant element, first outer race and housing define at a pressure chamber. The first outer race axially slidable relative to the second outer race such that an increase in pressure in pressure chamber causes a change in axial spacing between the outer races. This induces an additional axial load on the bearings which helps balance thrust load sharing.

First claim

What is claimed is:

1. A stacked bearing structure comprising:
a first bearing having a first inner race, a first outer race, and a first set of roller elements housed between the first inner race and the first outer race;
a second bearing having a second inner race, a second outer race, and a second set of roller elements housed between the second inner race and the second outer race;
a housing surrounding the first and second bearings; and
a first compliant element fixedly connected to the first outer race, the first compliant element connected between the housing and the first outer race;
a second compliant element fixedly connected to the second outer race, the second compliant element connected between the housing and the second outer race, wherein:
the first compliant element, first outer race, and the housing define a pressure chamber; and
the first outer race is axially slidable relative to the second outer race such that an increase in pressure in the pressure chamber causes a change in axial spacing between the first and second outer races.

2. The stacked bearing structure according to claim 1 , wherein:
the first and second compliant elements are provided at opposing axial ends of the stacked bearing structure; and
the first and second compliant elements, outer races, and the housing define a single pressure chamber.

3. The stacked bearing structure according to claim 2 , wherein the first outer race and the second outer race are slidably mounted to one another.

4. The stacked bearing structure according to claim 3 , wherein one of the first and second outer races includes an axial flange and another one of the first and second outer races includes an axial lip, the axial flange and the axial lip forming a sliding abutment.

5. The stacked bearing structure according to claim 1 , wherein:
the first compliant element, first outer race, and the housing define a first pressure chamber; and
the second compliant element, second outer race, and the housing define a second pressure chamber.

6. The stacked bearing structure according to claim 5 , wherein the first compliant element is proximal to the second bearing, and the second compliant element is distal to the first bearing.

7. The stacked bearing structure according to claim 5 , wherein the first and second outer races are slidably mounted to the housing.

8. The stacked bearing structure according to claim 7 , wherein the housing includes a first radial extension against which the first outer race is slidably mounted, and a second radial extension against which the second outer race is slidably mounted.

9. The stacked bearing structure according to claim 1 , wherein the first and second compliant elements are slidably mounted to the housing.

10. The stacked bearing structure according to claimed 9 , wherein the housing includes a first groove for locating a radially outer end of the first compliant element, and a second groove for locating a radially outer end of the second compliant element.

11. The stacked bearing structure according to claim 10 , wherein the first and second grooves have an axial extension that is greater than the axial extension of the radially outer ends of each of the first and second compliant elements so that the radially outer ends of the first and second compliant elements respectively slide within the first and second grooves.

12. The stacked bearing structure according to claim 1 , further comprising a valved pressure inlet or a respective valved pressure inlet extending through the housing to provide fluid communication from a pressure source to the, or the respective, pressure chamber.

13. The stacked bearing structure according to claim 1 , further comprising a valved pressure outlet or a respective valved pressure outlet extending through the housing to allow venting of pressure from within the, or the respective, pressure chamber.

14. The stacked bearing structure according to claim 1 , further comprising at least one load sensor associated with each of the first bearing and the second bearing.

15. The stacked bearing structure according to claim 14 , further comprising an electronic control module, the at least one load sensor is configured to monitor axial loads on each of the first and second bearings to provide feedback to the electronic control module.

16. The stacked bearing structure according to claim 15 , wherein the electronic control module is configured to trigger pressurisation of the pressure chamber in response to the axial load on the first bearing or the second bearing being below a predetermined minimum value.

17. The stacked bearing structure according to claim 15 , wherein the at least one load sensor and the electronic control module are configured to trigger venting of the pressure chamber.

18. A gas turbine engine comprising the stacked bearing structure as claimed in claim 1 .

19. The stacked bearing structure according to claim 1 , wherein the first compliant element is a flexible diaphragm and the second compliant element is a flexible diaphragm.

Assignees

• Rolls Royce Plc

Inventors

• Gallimore Stephen
• Fletcher Paul
• Peters Philip

Classifications

• F16C25/08

  self-adjusting · CPC title

• F16C19/16

  with a single row of balls · CPC title

• F16C19/06

  with a single row or balls · CPC title

• F16C41/02 Primary

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

• F02C7/06

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title