IP Library › Granted Patent US 11,454,320
Granted Patent B2
US 11,454,320 · App. 16/859,409 · Granted Sep 27, 2022

Porous seal element with internal fluid passage

Inventors: Benjamin Nasman (Tolland, CT); Michael M. Davis (North Granby, CT)
Assignee: Raytheon Technologies Corporation
F16J15/162F01D11/006F01D25/183F05D2220/32F05D2240/50F05D2240/55
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,454,320
App. No.
16/859,409
Granted
Sep 27, 2022
Kind
B2
Abstract

An assembly is provided for rotational equipment. This assembly includes a seal land and a seal element. The seal land extends circumferentially around and is configured to rotate about an axial centerline. The seal element is abutted against and is sealingly engaged with the seal land. The seal element extends circumferentially around the axial centerline. The seal element includes porous material, an exterior surface and a seal element passage. The seal element is configured to flow lubricant from the seal element passage, through the porous material, to the exterior surface.

Claims (51)

1. An assembly for rotational equipment, comprising:

a seal land extending circumferentially around and configured to rotate about an axial centerline;

a seal element adjacent and sealingly engaged with the seal land, the seal element extending circumferentially around the axial centerline, and the seal element comprising porous material, an exterior surface and a seal element passage, wherein the seal element is configured to flow lubricant from the seal element passage, through the porous material, to the exterior surface;

a guide rail; and

a seal carrier mated with and translatable along the guide rail;

the seal element mounted to the seal carrier.

2. The assembly of claim 1 , wherein

the seal land comprises a seal land surface; and

the exterior surface is abutted against and sealingly engages the seal land surface.

3. The assembly of claim 1 , wherein the seal element comprises a porous carbon seal element.

4. The assembly of claim 1 , wherein the seal element passage extends partially into the seal element to a blind passage end.

5. The assembly of claim 1 , wherein

the seal element passage comprises a plurality of apertures arranged circumferentially about the axial centerline; and

the seal element is configured to direct the lubricant from the each of the plurality of apertures, through the porous material, to the exterior surface.

6. The assembly of claim 1 , further comprising a non-porous coating applied to a second exterior surface of the seal element.

7. The assembly of claim 1 , further comprising a lubricant source configured to supply the lubricant to the seal element passage.

8. The assembly of claim 1 , further comprising:

a static structure of a gas turbine engine, the seal element non-rotatably coupled to the static structure; and

a rotating structure of the gas turbine engine, the seal land configured to rotate with the rotating structure;

wherein the rotational equipment comprises the gas turbine engine.

9. An assembly for rotational equipment, comprising:

a seal land extending circumferentially around and configured to rotate about an axial centerline;

a seal element adjacent and sealingly engaged with the seal land, the seal element extending circumferentially around the axial centerline, and the seal element comprising porous material, an exterior surface and a seal element passage, wherein the seal element is configured to flow lubricant from the seal element passage, through the porous material, to the exterior surface;

a guide rail configured with a guide rail passage; and

a seal support structure mated with and translatable along the guide rail;

the seal element mounted to the seal support structure; and

the seal element passage fluidly coupled with the guide rail passage through the seal support structure.

10. The assembly of claim 9 , further comprising a spring element engaged with the seal support structure and configured to bias the seal element against the seal land.

11. The assembly of claim 9 , further comprising:

a plurality of guide rails comprising the guide rail, the plurality of guide rails arranged in an array about the axial centerline; and

the seal support structure mated with and slidable along each of the plurality of guide rails.

12. The assembly of claim 9 , wherein

the seal support structure comprises a seal carrier and a fluid coupling device;

the seal carrier is mated with and slidable along the guide rail, and the seal carrier comprises a carrier passage that is fluidly coupled with the seal element passage; and

the fluid coupling device is mounted to and translatable along the guide rail, and the fluid coupling device comprises a coupling device passage that fluidly couples the guide rail passage with the carrier passage.

13. The assembly of claim 12 , wherein the fluid coupling device is configured to move relative to the seal carrier.

14. The assembly of claim 12 , wherein

the fluid coupling device includes a sleeve and a tube;

the sleeve is mounted to and translatable along the guide rail; and

the tube projects out from the sleeve and into a receptacle of the seal carrier.

15. The assembly of claim 12 , wherein the carrier passage includes an annular slot that interfaces with an inlet of the seal element passage.

16. The assembly of claim 12 , wherein

the seal carrier includes a flange; and

the guide rail projects through an aperture in the flange.

17. An assembly for rotational equipment, comprising:

a guide rail;

a seal carrier configured to translate along the guide rail, the seal carrier including a base and a flange projecting out from the base, and the flange comprising an aperture through which the guide rail projects; and

a seal element mounted to the base, the seal element comprising porous material, an exterior surface and a seal element passage, wherein the seal element is configured to flow lubricant from the seal element passage, through the porous material, to the exterior surface.

18. The assembly of claim 17 , wherein

the guide rail comprises a guide rail passage; and

the seal element passage is fluidly coupled with and configured to receive the lubricant from the guide rail passage.

Assignments (2)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 27, 2020
From: NASMAN, BENJAMIN; DAVIS, MICHAEL M.
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 052503/0555 →
Continuity (1)
Related Publication 20210332889A1 · Oct 28, 2021