Turbomachine with thrust bearing seal plate housing member having working fluid flow aperture

Patent metadata

Field	Value
Publication number	US-12345170-B2
Application number	US-202318351598-A
Country	US
Kind code	B2
Filing date	Jul 13, 2023
Priority date	Jun 1, 2023
Publication date	Jul 1, 2025
Grant date	Jul 1, 2025

Abstract

A turbomachine includes a housing, a rotating group that is housed within the housing, and a fluid bearing system with a thrust member. The turbomachine further includes a compressor stage configured to receive a fluid from an area within the housing. Also, the turbomachine includes a seal plate of the housing. The seal plate includes a first face and a second face. The first face has a flow surface that at least partly defines a fluid flow path toward the compressor wheel. The second face has a thrust member support surface configured to support the thrust member during rotation of the rotating group. The seal plate includes an aperture that fluidly connects the area to the fluid flow path.

First claim

What is claimed is:

1. A turbomachine comprising:
a housing;
a rotating group that is housed within the housing;
a fluid bearing system with a thrust bearing member fixed to the rotating group, the fluid bearing system configured to support the rotating group for rotation within the housing about an axis with the thrust bearing member configured to support the rotating group against thrust loads;
a compressor stage that includes a compressor wheel of the rotating group that is housed within a compressor housing of the housing, the compressor stage configured to receive a fluid from an area within the housing;
a seal plate of the housing, the seal plate including a first face and a second face, the first face having a flow surface that at least partly defines a fluid flow path toward the compressor wheel, the second face having a thrust bearing member support surface; and a wall portion of the housing, the seal plate attached to the wall portion to cooperatively encapsulate the thrust bearing member for rotation therebetween; wherein the wall portion has a recessed surface that defines a thrust pocket that receives the thrust bearing member, the thrust bearing member support surface covering over the thrust pocket and the thrust bearing member; the seal plate including an aperture arranged radially outwards of the thrust pocket that fluidly connects the area to the fluid flow path.

2. The turbomachine of claim 1 , wherein the flow surface is concavely contoured.

3. The turbomachine of claim 2 , wherein the first face includes an outer radial portion that faces axially along the axis, and wherein the first face includes an inner radial portion that curves and projects axially as the inner radial portion extends away from the outer radial portion.

4. The turbomachine of claim 3 , wherein the rotating group includes an extension that is received in the seal plate, the extension including an extension flow surface that is disposed in a downstream direction from the flow surface of the seal plate, the extension flow surface further defining the fluid flow path toward the compressor wheel.

5. The turbomachine of claim 4 , wherein the fluid flow path turns inward radially along the flow surface of the seal plate, and wherein the fluid flow path turns axially along the extension flow surface.

6. The turbomachine of claim 1 , wherein the aperture is a through-hole extending through the seal plate.

7. The turbomachine of claim 1 , wherein the housing includes a motor cavity that houses an e-machine, the aperture fluidly connecting the motor cavity to the fluid flow path.

8. The turbomachine of claim 1 , wherein the wall portion includes a recess defined by the recessed surface, the recess including an inlet area with a fluid inlet to the thrust pocket;
wherein the thrust pocket is substantially centered on the axis and the inlet area is eccentric to the axis.

9. The turbomachine of claim 8 , wherein the thrust bearing member support surface is flat and continuously covers the inlet area and the thrust pocket.

10. The turbomachine of claim 9 , further comprising a compressible seal member that continuously extends about the inlet area and the thrust pocket and seals between the seal plate and the wall portion.

11. The turbomachine of claim 1 , wherein the seal plate includes an inner radial surface that is smooth; and
wherein the rotating group includes a plurality of seal features that cooperatively defines, with the inner radial surface, a labyrinthine seal along the axis between the rotating group and the housing.

12. The turbomachine of claim 1 , wherein the compressor stage is a first compressor stage; and
further comprising a second compressor stage cooperatively defined by the housing and the rotating group, the second compressor stage configured to receive the fluid from the first compressor stage.

13. A method of manufacturing a turbomachine comprising:
providing a housing;
providing a rotating group;
housing the rotating group within the housing; and
supporting, with a fluid bearing system, the rotating group within the housing for rotation about an axis of rotation, the fluid bearing system including a thrust bearing member fixed to the rotating group, the thrust bearing member configured to support the rotating group against thrust loads;
defining a compressor stage that includes a compressor wheel of the rotating group that is housed within a compressor housing of the housing, the compressor stage configured to receive a fluid from an area within the housing;
the housing including a seal plate that includes a first face and a second face, the first face having a flow surface that at least partly defines a fluid flow path toward the compressor wheel, the second face having a thrust bearing member support surface; the housing including a wall portion; and attaching the seal plate to the wall portion to cooperatively encapsulate the thrust bearing member for rotation therebetween; wherein the wall portion has a recessed surface that defines a thrust pocket that receives the thrust bearing member, the thrust bearing member support surface covering over the thrust pocket and the thrust bearing member; the seal plate including an aperture arranged radially outwards of the thrust pocket that fluidly connects the area to the fluid flow path.

14. The method of claim 13 , wherein the flow surface is concavely contoured.

15. The method of claim 14 , wherein the first face includes an outer radial portion that faces axially along the axis, and wherein the first face includes an inner radial portion that curves and projects axially as the inner radial portion extends away from the outer radial portion.

16. The method of claim 15 , wherein the rotating group includes an extension that is received in the seal plate, the extension including an extension flow surface that is disposed in a downstream direction from the flow surface of the seal plate, the extension flow surface further defining the fluid flow path toward the compressor wheel.

17. The method of claim 16 , wherein the fluid flow path turns inward radially along the flow surface of the seal plate, and wherein the fluid flow path turns axially along the extension flow surface.

18. The method of claim 13 , wherein the aperture is a through-hole extending through the seal plate.

19. A compressor device comprising:
a housing;
a rotating group that is housed within the housing, the rotating group and the housing cooperating to define a first compressor stage and a second compressor stage;
a fluid bearing system with a thrust bearing member, the fluid bearing system fixed to the rotating group, the fluid bearing system configured to support the rotating group for rotation within the housing about an axis with, the thrust bearing member configured to support the rotating group against thrust loads;
a motor stage including an electric motor included in a motor cavity of the housing, the electric motor operatively connected to the rotating group for driving rotation thereof;
the first compressor stage including a first compressor wheel of the rotating group that is housed within a first compressor housing of the housing, the first compressor stage configured to receive a fluid from an area within the housing;
the second compressor stage including a second compressor wheel of the rotating group that is housed within a second compressor housing of the housing, the second compressor stage configured to receive the fluid from the first compressor stage;
a seal plate of the housing, the s

Assignees

• Garrett Transportation I Inc

Inventors

• Nazare Kiran Somashekar Rao
• John Poomkuzhimannil
• Kopecky Matej

Classifications

• F05D2240/55

  Seals · CPC title

• F05D2240/52

  Axial thrust bearings · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title

• F04D25/06

  the pump being electrically driven (F04D25/08 takes precedence) · CPC title