Oil control for seal plates

Patent metadata

Field	Value
Publication number	US-10655679-B2
Application number	US-201715481934-A
Country	US
Kind code	B2
Filing date	Apr 7, 2017
Priority date	Apr 7, 2017
Publication date	May 19, 2020
Grant date	May 19, 2020

Abstract

A seal assembly for a bearing compartment of a gas turbine engine includes a seal carrier, a seal element, a seal plate, and a trough. At least a portion of the seal element is within the seal carrier. The seal plate is in contact with the seal element and is configured to rotate relative to the seal element. The trough extends around the seal plate and comprises an annular channel positioned to capture oil slung from the seal plate.

First claim

The invention claimed is:

1. A seal assembly for a bearing compartment of a gas turbine engine, the seal assembly comprising:
a seal carrier;
a seal element, wherein at least a portion of the seal element is within the seal carrier;
a seal plate in contact with the seal element, wherein the seal plate is configured to rotate relative to the seal element; and
a trough extending around the seal plate, wherein the trough comprises:
a wall with a U-shaped cross-section and an annular configuration; and
an annular channel formed by the U-shape of the wall, wherein the annular channel is positioned radially outward from the seal plate so as to capture oil slung from the seal plate.

2. The seal assembly of claim 1 , wherein the trough is disposed concentrically with the seal plate.

3. The seal assembly of claim 1 , wherein a mounting feature is attached to and extends from the trough.

4. The seal assembly of claim 1 further comprising a screen disposed in the annular channel of the trough.

5. The seal assembly of claim 4 , wherein the screen comprises perforations and is configured to separate the oil captured by the trough from windage produced by the seal plate.

6. The seal assembly of claim 1 further comprising an exit forming an outlet passage, wherein the exit is a hollow tube that is connected to the wall of the trough, wherein the outlet passage formed by the exit is fluidly connected to the annular channel of the trough.

7. A method of controlling oil flow within a bearing compartment of a gas turbine engine, the method comprising:
rotating a seal plate relative to a seal element affixed to the bearing compartment, wherein the seal plate is attached to a shaft of the gas turbine engine;
slinging oil from the rotating seal plate;
capturing the oil slung from the seal plate in an annular channel of a trough surrounding the seal plate, wherein the trough comprises:
a wall with a U-shaped cross-section and an annular configuration; and
an annular channel formed by the U-shape of the wall, wherein the annular channel is positioned radially outward from the seal plate so as to capture oil slung from the seal plate;

directing the captured oil to an exit that forms an outlet passage, wherein the exit is a hollow tube that is connected to the wall of the trough, wherein the outlet passage formed by the exit is fluidly connected to the annular channel of the trough; and
draining the captured oil through the exit.

8. The method of claim 7 further comprising:
preventing the oil slung from the seal plate from impinging gears located in the bearing compartment.

9. The method of claim 7 further comprising:
separating the oil from windage produced by the seal plate with a screen disposed in the annular channel of the trough.

10. The method of claim 7 , wherein slinging the oil from the rotating seal plate comprises discharging the oil from a communication hole disposed in the rotating seal plate.

11. The method of claim 7 , further comprising directing the oil drained from the exit to a scavenge port of the bearing compartment.

Assignees

• United Technologies Corp

Inventors

• Anglin Christopher T
• Messerschmidt Dwayne E
• Valva Christopher M
• Gaulin Todd M

Classifications

• F16C27/045

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

• F16C33/78 Primary

  with a diaphragm, disc, or ring, with or without resilient members {(F16C33/761 takes precedence)} · CPC title

• F16C19/06

  with a single row or balls · CPC title

• F05D2240/70

  Slinger plates or washers · CPC title

• F16C2360/23

  Gas turbine engines · CPC title