Non-linear bumper bearings

Patent metadata

Field	Value
Publication number	US-10309256-B2
Application number	US-201415029494-A
Country	US
Kind code	B2
Filing date	Oct 10, 2014
Priority date	Oct 15, 2013
Publication date	Jun 4, 2019
Grant date	Jun 4, 2019

Abstract

A bumper bearing assembly includes a bearing housing having a level of radial spring stiffness, wherein the bearing housing defines a bearing seat. A bumper bearing is connected to the bearing housing by a spring having a level of radial spring stiffness lower than that of the bearing housing. The bumper bearing is configured to apply the level of radial spring stiffness of the spring against a rotor with the bumper bearing spaced apart from the bearing seat. The bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the bumper bearing seated against the bearing seat.

First claim

What is claimed is:

1. A bumper bearing assembly comprising:
a bearing housing having a level of radial spring stiffness, wherein the bearing housing defines a first bearing seat and a second bearing seat; and
a bumper bearing connected to the bearing housing by a spring having a level of radial spring stiffness lower than that of the bearing housing, wherein the bumper bearing is configured to apply the level of radial spring stiffness of the spring against a rotor with the bumper bearing spaced apart from the first bearing seat, and wherein the bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the bumper bearing seated against the first bearing seat; and
a second bumper bearing opposed to the bumper bearing and connected to the bearing housing by a second spring having a level of radial spring stiffness lower than that of the bearing housing, wherein the second bumper bearing is positioned to apply the level of radial spring stiffness of the second spring in a second radial direction opposed to the first radial direction against the rotor with the second bumper bearing spaced apart from the second bearing seat, and wherein the bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the second bumper bearing seated against the second bearing seat, wherein each of the first and second bumper bearings is individually tuned so the first and second bumper bearings differ from one another in respective level of radial spring stiffness of the bearing housing.

2. The bumper bearing assembly as recited in claim 1 , wherein the bumper bearing and bearing seat are arcuate.

3. The bumper bearing assembly as recited in claim 1 , wherein the bumper bearing includes a coating on a bearing surface opposite the bearing seat, wherein the coating is configured to engage the rotor rotating relative to the bearing seat.

4. The bumper bearing assembly as recited in claim 1 , further comprising an anti-rotation lug at one end of the bearing seat and engaged to limit circumferential rotation of the bumper bearing.

5. The bumper bearing assembly as recited in claim 1 , wherein the bumper bearing includes a plurality of circumferentially spaced bumper segments each connected to the bearing housing with a respective spring including the a level of radial spring stiffness lower than that of the bearing housing.

6. The bumper bearing assembly as recited in claim 5 , wherein an anti-rotation lug is disposed between each circumferentially adjacent pair of bumper segments.

7. The bumper bearing assembly as recited in claim 5 , wherein the bumper segments substantially surround a rotor passage through the bearing housing.

8. A gas turbine engine comprising:
a casing;
a rotor mounted for rotation about a longitudinal axis relative to the casing; and
a bumper bearing assembly mounted to the casing, the bumper bearing assembly including:
a bearing housing having a level of radial spring stiffness, wherein the bearing housing defines first and second bearing seats;
a first bumper bearing connected to the bearing housing by a first spring having a level of radial spring stiffness lower than that of the bearing housing, wherein the first bumper bearing is positioned to apply the level of radial spring stiffness of the first spring in a first radial direction against the rotor with the first bumper bearing spaced apart from the first bearing seat, and wherein the bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the first bumper bearing seated against the first bearing seat; and
a second bumper bearing opposed to the first bumper bearing and connected to the bearing housing by a second spring having a level of radial spring stiffness lower than that of the bearing housing, wherein the second bumper bearing is positioned to apply the level of radial spring stiffness of the second spring in a second radial direction opposed to the first radial direction against the rotor with the second bumper bearing spaced apart from the second bearing seat, and wherein the bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the second bumper bearing seated against the second bearing seat, wherein each of the first and second bumper bearings is individually tuned so the first and second bumper bearings differ from one another in respective level of radial spring stiffness of the bearing housing.

9. The gas turbine engine as recited in claim 8 , wherein the first and second bearing seats are spaced apart from one another axially relative to the longitudinal axis for counteracting thermally induced warpage in the rotor.

10. The gas turbine engine as recited in claim 9 , wherein the first and second bumper bearings each have an arcuate inner surface for engaging the rotor, wherein the arcuate inner surfaces define a bearing radius, and wherein a bumper span is defined axially from a center of the first bumper bearing to a center of the second bumper bearing, and wherein the ratio of the bumper span to the bearing radius is between 1 and 5.

11. The gas turbine engine as recited in claim 8 , wherein the first and second bumper bearings each include a coating on a bearing surface configured to engage the rotor for rotation of the rotor relative to the first and second bearing seats.

12. The gas turbine engine as recited in claim 8 , further comprising a respective anti-rotation lug at one end of each bearing seat and engaged to limit circumferential rotation of a respective one of the first and second bumper bearings.

13. The gas turbine engine as recited in claim 8 , wherein each of the first and second bumper bearings includes a plurality of circumferentially spaced bumper segments each connected to the bearing housing with a respective spring.

14. The gas turbine engine as recited in claim 13 , wherein an anti-rotation lug is disposed between each circumferentially adjacent pair of bumper segments.

15. The gas turbine engine as recited in claim 13 , wherein the bumper segments substantially surround the rotor.

16. A bumper bearing assembly comprising:
a bearing housing having a level of radial spring stiffness, wherein the bearing housing defines first and second bearing seats;
a first bumper bearing connected to the bearing housing by a first spring having a level of radial spring stiffness lower than that of the bearing housing, wherein the first bumper bearing is positioned to apply the level of radial spring stiffness of the first spring in a first radial direction against a rotor with the first bumper bearing spaced apart from the first bearing seat, and wherein the bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the first bumper bearing seated against the first bearing seat; and
a second bumper bearing opposed to the first bumper bearing and connected to the bearing housing by a second spring having a level of radial spring stiffness lower than that of the bearing housing, wherein the second bumper bearing is positioned to apply the level of radial spring stiffness of the second spring in a second radial direction opposed to the first radial direction against the rotor with the second bumper bearing spaced apart from the second bearing seat, and wherein the bearing housing is configured to apply the level of radial spring stiffness of the bearing housing against the rotor with the second bumper bearing seat

Assignees

• United Technologies Corp
• United Tech Corpoation

Inventors

• Duong Loc Quang
• Hu Xiaolan

Classifications

• F16C33/108

  with a plurality of elements forming the bearing surfaces, e.g. bearing pads · CPC title

• F16C17/03

  with tiltably-supported segments, e.g. Michell bearings {(hydrostatic bearings with tiltably supported bearing pads F16C32/0666; made from a plurality of rods F16C33/26; with flexible leaves F16C17/024; hydrodynamic bearings with chambers F16C33/1075)} · CPC title

• F01D5/021

  for flow machines or engines with only one axial stage (for more than one stage F01D5/06) · CPC title

• F01D25/164 Primary

  Flexible supports; Vibration damping means associated with the bearing · CPC title

• F05D2220/32

  in gas turbines · CPC title