Rotational equipment seal element with internal fluid passage

Patent metadata

Field	Value
Publication number	US-11466778-B2
Application number	US-202016859374-A
Country	US
Kind code	B2
Filing date	Apr 27, 2020
Priority date	Apr 27, 2020
Publication date	Oct 11, 2022
Grant date	Oct 11, 2022

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 rotatable about an axial centerline. The seal land includes a seal land surface. The seal element extends circumferentially around the axial centerline. The seal element includes a seal element surface and a seal element passage. The seal element surface is abutted against and is sealingly engaged with the seal land surface. The seal element passage extends through the seal element to an interface between the seal element surface and the seal land surface.

First claim

What is claimed is:

1. An assembly for rotational equipment, comprising:
a seal land extending circumferentially around and rotatable about an axial centerline, the seal land comprising a seal land surface; and
a seal element extending circumferentially around the axial centerline, the seal element comprising a seal element surface and a seal element passage, the seal element surface abutted against and sealingly engaged with the seal land surface, and the seal element passage extending through the seal element to an interface between the seal element surface and the seal land surface;
the seal element passage extending axially within the seal element to an outlet in the seal element surface; and
the seal land further comprising a groove and an aperture, the groove arranged in the seal land surface radially displaced from the outlet, and the aperture fluidly coupled with the groove and extending through the seal land.

2. The assembly of claim 1 , wherein
the seal element further comprises a second seal element passage; and
the second seal element passage extends through the seal element to the interface between the seal element surface and the seal land surface.

3. The assembly of claim 1 , wherein the seal element comprises an annular carbon seal element.

4. The assembly of claim 1 , wherein
the seal element extends axially along the axial centerline between a seal element first end and a second element second end; and
the seal element surface is arranged at the seal element first end.

5. 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 rotatable with the rotating structure;
wherein the rotational equipment comprises the gas turbine engine.

6. The assembly of claim 1 , further comprising:
a guide rail; and
a seal carrier mated with and translatable along the guide rail;
the seal element mounted to the seal carrier.

7. An assembly for rotational equipment, comprising:
a seal land extending circumferentially around and rotatable about an axial centerline, the seal land comprising a seal land surface;
a seal element extending circumferentially around the axial centerline, the seal element comprising a seal element surface and a seal element passage, the seal element surface abutted against and sealingly engaged with the seal land surface, and the seal element passage extending through the seal element to an interface between the seal element surface and the seal land 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.

8. The assembly of claim 7 , further comprising a spring element configured to bias the seal element against the seal land.

9. The assembly of claim 7 , 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.

10. The assembly of claim 7 , 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 is configured with 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 is configured with a coupling device passage that fluidly couples the guide rail passage with the carrier passage.

11. The assembly of claim 10 , wherein the fluid coupling device is configured to move relative to the seal carrier.

12. The assembly of claim 10 , 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.

13. The assembly of claim 10 , wherein the carrier passage includes an annular slot that interfaces with an inlet of the seal element passage.

14. The assembly of claim 10 , wherein
the seal carrier includes a flange; and
the guide rail projects through a channel that extends radially into the flange.

15. The assembly of claim 7 , wherein
the seal element passage extends within the seal element to an outlet in the seal element surface; and
the seal land surface overlaps the outlet.

16. The assembly of claim 7 , 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 rotatable with the rotating structure;
wherein the rotational equipment comprises the gas turbine engine.

17. An assembly for rotational equipment, comprising:
a guide rail comprising a guide rail passage;
a seal carrier mated with and translatable along the guide rail; and
a seal element mounted to the seal carrier, the seal element comprising a seal element surface and a seal element passage that extends through the seal element to the seal element surface, wherein the seal element passage is fluidly coupled with the guide rail passage.

Assignees

• Raytheon Tech Corp

Inventors

• Nasman Benjamin
• Davis Michael M

Classifications

• F16J15/342 Primary

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

• F05D2220/32

  in gas turbines · CPC title

• F01D25/183

  Sealing means · CPC title

• F05D2240/50

  Bearings · CPC title

• F16J15/3404

  and characterised by parts or details relating to lubrication, cooling or venting of the seal · CPC title