Variable preloaded duplex thrust bearing system for a geared turbofan engine

Patent metadata

Field	Value
Publication number	US-9932986-B2
Application number	US-201615229423-A
Country	US
Kind code	B2
Filing date	Aug 5, 2016
Priority date	Aug 5, 2016
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

A bearing system for a gas turbine engine includes an outer housing and a first ball bearing assembly disposed radially inward from the outer housing relative a center axis of the outer housing. The bearing system also includes a second ball bearing assembly disposed radially inward from the outer housing and positioned axially aft of the first ball bearing assembly. The bearing system also includes a resilient member that is connected to the outer housing and compressed against at least one of a first outer race of the first ball bearing assembly and a second outer race of the second ball bearing assembly in an axial direction parallel to the center axis.

First claim

The invention claimed is:

1. A bearing system for a gas turbine engine comprises:
an outer housing comprising a forward end and an aft end;
a first ball bearing assembly disposed radially inward from the outer housing relative a center axis of the outer housing, wherein the first ball bearing assembly comprises:
a first outer race disposed radially inward from the outer housing;
a first inner race disposed radially inward from the first outer race; and
a first plurality of ball bearing elements disposed between the first outer race and the first inner race;

a second ball bearing assembly disposed radially inward from the outer housing and positioned axially aft of the first ball bearing assembly, wherein the second ball bearing assembly comprises:
a second outer race disposed radially inward from the outer housing;
a second inner race disposed radially inward from the second outer race; and
a second plurality of ball bearing elements disposed between the second outer race and the second inner race;

a resilient member connected to the outer housing, wherein the resilient member is compressed against at least one of the first outer race and the second outer race in an axial direction parallel to the center axis wherein the resilient member comprises:
a flange that extends radially relative the center axis;
a body that extends axially parallel to the center axis; and
a curved bow disposed radially inward from the flange and the body and
connecting the flange to the body.

2. The bearing system of claim 1 further comprising:
a bearing support cage comprising a forward end, an aft end, and a plurality of circumferentially spaced beams extending between the forward end and the aft end of the bearing support cage, wherein the aft end of the bearing support cage is connected to the forward end of the outer housing.

3. The bearing system of claim 1 , wherein the flange of the resilient member is connected to the forward end of the outer housing, the body is disposed radially between the outer housing and the first outer race, and the curved bow of the resilient member is disposed radially inward of the outer housing and forward of the first ball bearing assembly.

4. The bearing system of claim 3 , wherein the second ball bearing assembly is smaller in diameter than the first ball bearing assembly.

5. The bearing system of claim 4 , wherein the outer housing comprises a step-down portion disposed circumferentially around the second ball bearing assembly, wherein the step-down portion of the outer housing is smaller in diameter than a forward portion of the outer housing, wherein the forward portion of the outer housing is disposed circumferentially around the first ball bearing assembly.

6. The bearing system of claim 5 , wherein the bearing system further comprises:
a first fastener connected to an inner surface of the step-down portion of the outer housing, wherein the first fastener is positioned axially forward of the second ball bearing assembly and axially aft of the first ball bearing assembly.

7. The bearing system of claim 6 , wherein the bearing system further comprises:
a second fastener positioned radially outward of the first fastener and radially inward of an aft end of the body of the resilient member, wherein the second fastener is connected to the aft end of the body of the resilient member.

8. The bearing system of claim 7 , wherein the bearing system further comprises:
an anti-rotation washer that extends radially from the first fastener to the second fastener and is configured to prevent rotation between the first fastener and the second fastener,
wherein the first fastener and the second fastener are spanner nuts.

9. The bearing system of claim 8 , wherein the aft end of the outer housing comprises a stop face that extends radially inward from the step-down portion and contacts an aft end of the second outer race of the second ball bearing assembly.

10. A bearing system for a gas turbine engine comprises:
an outer housing comprising a forward end, an aft end, a first portion, and a second portion, wherein the first portion extends axially between the forward end of the outer housing and the second portion of the outer housing, wherein the second portion extends axially between the first portion and the aft end of the outer housing;
a first ball bearing assembly disposed radially inward from the outer housing relative a center axis of the outer housing, wherein the first ball bearing assembly comprises:
a first outer race disposed radially inward from the outer housing;
a first inner race disposed radially inward from the first outer race; and
a first plurality of ball bearing elements disposed between the first outer race and the first inner race;

a second ball bearing assembly disposed radially inward from the outer housing and positioned axially aft of the first ball bearing assembly, wherein the second ball bearing assembly comprises:
a second outer race disposed radially inward from the outer housing;
a second inner race disposed radially inward from the second outer race; and
a second plurality of ball bearing elements disposed between the second outer race and the second inner race;

a spring connected to the forward end of the outer housing by a fastener and contacting the first outer race, wherein the spring is compressed axially between the fastener and the first outer race, and wherein the spring comprises:
a flange that extends radially inward from the forward end of the outer housing relative the center axis;
a body disposed axially aft of the flange, wherein the body extends axially parallel to the center axis and is disposed radially between the first outer race and the first portion of the outer housing; and
a curved bow disposed radially inward from the flange and the body and connecting the flange to the body.

11. The bearing system of claim 10 , wherein the second portion is smaller in diameter than the first portion.

12. The bearing system of claim 11 , wherein the second outer race, the second inner race, and the second plurality of ball bearing elements are smaller in diameter than the first outer race, the first inner race, and the first plurality of ball bearing elements respectively.

13. The bearing system of claim 12 , wherein the first portion of the outer housing is disposed around the first ball bearing assembly and the second portion of the outer housing is disposed around the second ball bearing assembly.

14. The bearing system of claim 13 further comprising:
a bearing support cage comprising a forward end, an aft end, and a plurality of circumferentially spaced beams extending between the forward end and the aft end of the bearing support cage, wherein the aft end of the bearing support cage is connected to the forward end of the outer housing.

15. The bearing system of claim 14 , wherein the bearing support cage is disposed radially outward from the outer housing relative the center axis.

16. A bearing system for a gas turbine engine comprises:
a radial spring;
an outer housing comprising a forward end and an aft end, wherein the forward end of the outer housing is connected to the radial spring;
a first ball bearing assembly disposed radially inward from the outer housing relative a center axis of the outer housing, wherein the first ball bearing assembly comprises:
a first outer race disposed radially inward from the outer housing;
a first inner race disposed radially inward from the first outer race; and
a first plurality of ball bearing elements disposed between the first outer race and the fir

Assignees

• United Technologies Corp

Inventors

• Dibenedetto Enzo

Classifications

• F16C27/045

  with a fluid film, e.g. squeeze film damping · CPC title

• F04D29/059

  Roller bearings · CPC title

• F04D29/051 Primary

  Axial thrust balancing · CPC title

• F16C27/08

  primarily for axial load, e.g. for vertically-arranged shafts · CPC title

• F16C25/083

  with resilient means acting axially on a race ring to preload the bearing · CPC title