Shield for arranging between a bearing and a rotating seal element

Patent metadata

Field	Value
Publication number	US-10344679-B2
Application number	US-201414775808-A
Country	US
Kind code	B2
Filing date	Mar 14, 2014
Priority date	Mar 15, 2013
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

An assembly is provided that includes a shaft, a bearing, a stator seal element, a rotor seal element and a shield. The shaft extends along an axis. The bearing supports the shaft and receives lubrication fluid. The stator seal element circumscribes the shaft. The rotor seal element is mounted on the shaft axially between the bearing and the stator seal element. The rotor seal element forms a seal with the stator seal element. The shield substantially prevents the lubrication fluid from traveling axially away from the bearing onto the rotor seal element.

First claim

What is claimed is:

1. A turbine engine assembly, comprising:
a turbine engine shaft extending along an axis;
a bearing including an inner race and an outer race, wherein the inner race is mounted on the shaft and is separated from the outer race by a gap;
a rotor seal element mounted on the shaft;
a shield blocking all axial lines of sight between the gap and the rotor seal element; and
an annular stator seal element that axially engages and forms a seal with the rotor seal element, the rotor seal element arranged axially between the shield and the stator seal element.

2. The assembly of claim 1 , wherein the rotor seal element includes a seal surface that faces away from the bearing.

3. The assembly of claim 1 , wherein the shield comprises an annular rotor shield that is mounted on the shaft axially between the inner race and the rotor seal element.

4. The assembly of claim 3 , wherein
the inner race extends radially outward to an outer surface with a first radius;
the outer race extends radially inward to an inner surface with a second radius; and
the shield extends radially outward to an outer surface with a third radius that is greater than the first radius and less than the second radius.

5. The assembly of claim 3 , wherein
the outer race extends radially inward to an inner surface with a first radius; and
the shield extends radially outward to an outer surface with a second radius that is one of equal to and greater than the first radius.

6. The assembly of claim 3 , wherein the shield includes a sleeve and an annular flange, the sleeve is mounted on the shaft, and the flange blocks the axial line of sight between the gap and the rotor seal element.

7. The assembly of claim 3 , wherein the shield axially engages at least one of the inner race and the rotor seal element.

8. The assembly of claim 3 , further comprising a spacer mounted on the shaft axially between the shield and one of the inner race and the rotor seal element.

9. The assembly of claim 1 , wherein
the inner race extends radially outward to an outer surface with a first radius;
the outer race extends radially inward to an inner surface with a second radius; and
the shield comprises a stator shield that extends radially inward to an inner surface with a third radius that is greater than the first radius and less than the second radius.

10. The assembly of claim 1 , wherein
the inner race extends radially outward to an outer surface with a first radius; and
the shield comprises a stator shield that extends radially inward to an inner surface with a second radius that is one of equal to and less than the first radius.

11. The assembly of claim 1 , wherein the stator seal element comprises a lift-off face seal, and the rotor seal element comprises a face seal landing.

12. The assembly of claim 1 , wherein
the shield comprises an annular disk;
the annular disk extends axially between opposing annular and planar side surfaces;
the annular disk extends radially to a cylindrical end surface; and
the cylindrical end surface respectively meets with the opposing annular and planar side surfaces at corners of the annular disk.

13. An assembly, comprising:
a shaft extending along an axis;
a bearing supporting the shaft, and receiving lubrication fluid;
a stator seal element circumscribing the shaft;
a rotor seal element mounted on the shaft axially between the bearing and the stator seal element, the rotor seal element axially engaging and forming a seal with the stator seal element; and
a shield comprising an annular disk configured to prevent the lubrication fluid from traveling axially away from the bearing onto the rotor seal element;
the annular disk extending axially between opposing disk side surfaces, and the annular disk extending radially to a disk end surface, wherein the disk end surface extends axially between and is contiguous with the opposing disk side surfaces.

14. The assembly of claim 13 , wherein
the bearing includes an inner race and an outer race, and the inner race is mounted on the shaft and is separated from the outer race by a gap; and
the shield blocks an axial line of sight between the gap and the rotor seal element.

15. The assembly of claim 13 , wherein
the bearing includes an inner race and an outer race, and the inner race is mounted on the shaft and is separated from the outer race by a gap; and
the shield further includes a sleeve mounted on the shaft, and the annular disk is connected to and projects radially from the sleeve.

16. The assembly of claim 13 , wherein
the bearing includes an inner race and an outer race;
the inner race extends radially outward to an outer surface with a first radius;
the outer race extends radially inward to an inner surface with a second radius; and
the shield is mounted on the shaft axially between the inner race and the rotor seal element, and the annular disk extends radially outward to the disk end surface with a third radius that is greater than the first radius and less than the second radius.

17. The assembly of claim 13 , wherein
the bearing includes an outer race that extends radially inward to an inner surface with a first radius; and
the shield is mounted on the shaft axially between the inner race and the rotor seal element, and the annular disk extends radially outward to the disk end surface with a second radius that is one of equal to and greater than the first radius.

18. A turbine engine assembly, comprising:
a housing defining an annular chamber;
a turbine engine shaft extending along an axis into the chamber;
a bearing supporting the shaft within the chamber, and including an inner race and an outer race that is separated from the inner race by a gap;
a rotor seal element mounted on the shaft within the chamber, the rotor seal element including a seal surface that faces away from the bearing; and
a shield including a sleeve and a flange, wherein the sleeve is mounted on the shaft axially between the bearing and the rotor seal element, and the flange extends radially from the sleeve to a distal end surface and blocks a line of sight into the gap;
wherein a first axial thickness of the flange at an interface between flange and the shield is equal to a second axial thickness of the flange at the distal end surface.

19. The assembly of claim 18 , wherein
the bearing receives lubrication fluid; and
the flange prevents the lubrication fluid from traveling out of the bearing onto the rotor seal element.

20. The assembly of claim 18 , wherein
the inner race extends radially outward to an outer surface with a first radius; and
the flange extends radially outward to an outer surface with a second radius that is greater than the first radius.

Assignees

• United Technologies Corp

Inventors

• James Denman H

Classifications

• F16J15/342

  with means for feeding fluid directly to the face · CPC title

• F01D25/183

  Sealing means · CPC title

• F16J15/3452

  the pressing force resulting from the action of a spring · CPC title

• F05D2260/941

  particularly aimed at mechanical or thermal stress reduction · CPC title

• F05D2260/231

  Preventing heat transfer · CPC title