Turbine bearing and seal assembly for a turbocharger

Patent metadata

Field	Value
Publication number	US-9803493-B2
Application number	US-201414503875-A
Country	US
Kind code	B2
Filing date	Oct 1, 2014
Priority date	Oct 1, 2014
Publication date	Oct 31, 2017
Grant date	Oct 31, 2017

Abstract

A turbine bearing and seal assembly is disclosed. The turbine bearing and seal assembly may have a turbine cartridge. The turbine cartridge may have a compressor end and a turbine end opposite the compressor end. The turbine bearing and seal assembly may also have a bearing attached to the turbine cartridge. The bearing may be disposed between the compressor end and the turbine end. The turbine bearing and seal assembly may further have a seal collar attachable to a shaft. The seal collar may be disposed within the turbine cartridge adjacent the turbine end.

First claim

What is claimed is:

1. A turbine bearing and seal assembly, comprising:
a turbine cartridge having a compressor end and a turbine end opposite the compressor end;
a bearing aligned with the turbine cartridge, the bearing being disposed between the compressor end and the turbine end; and
a seal collar attachable to a shaft, the seal collar being disposed within the turbine cartridge, the seal collar extending from a front end disposed adjacent the turbine end to a rear end disposed between the turbine end and the compressor end, the seal collar including:
a step seal disposed adjacent the front end, the step seal having a conical outer surface; and
a labyrinth seal disposed adjacent the rear end.

2. The turbine bearing and seal assembly of claim 1 , wherein the turbine cartridge includes a mounting flange disposed between the compressor end and the turbine end, the mounting flange being configured to engage with a bearing housing.

3. The turbine bearing and seal assembly of claim 1 , wherein the step seal and the labyrinth seal are configured to be charged with compressed air received from a compressor housing associated with the turbine bearing and seal assembly.

4. The turbine bearing and seal assembly of claim 3 , wherein the labyrinth seal includes:
a cylindrical outer surface; and
projections extending radially outward from the outer surface, the projections being axially spaced apart from each other.

5. The turbine bearing and seal assembly of claim 4 , wherein an inner surface of the third cartridge bore of the turbine cartridge is separated from the projections by an annular gap.

6. The turbine bearing and seal assembly of claim 3 , wherein the step seal includes:
projections extending radially outward from the outer surface, the projections being axially spaced apart from each other.

7. The turbine bearing and seal assembly of claim 6 , wherein
inner surfaces of the first annular bore and the second annular bore are separated from the projections by corresponding annular gaps; and
the projections cooperate with the inner surfaces to form cavities.

8. The turbine bearing and seal assembly of claim 7 , wherein each of the cavities includes:
an upper cavity;
a lower cavity axially offset from the upper cavity;
an inlet located at a first cavity end, the inlet being located an inlet radius;
an outlet located at a second cavity end opposite the first cavity end, the outlet being located at an outlet radius larger than the inlet radius.

9. The turbine bearing and seal assembly of claim 1 , wherein the turbine cartridge includes:
a first cartridge bore adjacent the compressor end, the first cartridge bore having a conical inner surface extending from the compressor end to a first distal end within the turbine cartridge; and
a second cartridge bore adjacent the turbine end, the second cartridge bore having a conical shape extending from the turbine end to a second distal end within the turbine cartridge, the second cartridge bore being configured to receive the seal collar.

10. The turbine bearing and seal assembly of claim 9 , wherein the turbine cartridge includes a third cartridge bore disposed between the first cartridge bore and the second cartridge bore, the third cartridge bore having a cylindrical shape and being configured to receive the bearing.

11. The turbine bearing and seal assembly of claim 10 , wherein the third cartridge bore includes:
an annular recess; and
a plurality of baffles extending radially inward from an inner surface of the annular recess.

12. The turbine bearing and seal assembly of claim 10 , wherein the second cartridge bore includes:
at least a first annular bore disposed at a first axial distance from the second distal end, the first annular bore having a first radius; and
at least a second annular bore disposed at a second axial distance from the second distal end, the second axial distance being larger than the first axial distance, the second annular bore having a second radius larger than the first radius.

13. A turbocharger, comprising:
a turbine housing;
a turbine wheel disposed within the turbine housing and configured to be rotated by exhaust received from an engine;
a compressor housing;
a shaft attached to the turbine wheel, the shaft extending from the turbine housing to the compressor housing;
a compressor impeller disposed within the compressor housing, the compressor impeller being disposed on the shaft and configured to be driven by the turbine wheel;
a bearing housing disposed coaxially with the shaft;
a turbine cartridge disposed within the bearing housing, the turbine cartridge including:
a compressor end;
a turbine end opposite the compressor end;
a first cartridge bore extending from the compressor end to a first distal end within the turbine cartridge, the first cartridge bore having a conical inner surface;
a second cartridge bore extending from the turbine end to a second distal end within the turbine cartridge, the second cartridge bore having a conical shape; and
a third cartridge bore disposed between the first cartridge bore and the second cartridge bore, the third cartridge bore having a cylindrical shape;

a bearing disposed within the third cartridge bore of the turbine cartridge, the bearing being configured to support the shaft; and
a seal collar attached to the shaft, the seal collar being disposed within the turbine cartridge, the seal collar extending from a front end disposed adjacent the turbine end to a rear end disposed between the turbine end and the compressor end, the seal collar including:
a step seal disposed adjacent the front end, the step seal having a conical outer surface; and
a labyrinth seal disposed adjacent the rear end.

14. The turbocharger of claim 13 , wherein the step seal and the labyrinth seal are configured to be charged with compressed air from the compressor housing.

Assignees

• Electro Motive Diesel Inc

Inventors

• Svihla Gary R
• Rexavier Raji
• Schueler Joshua D

Classifications

• F01D25/186

  for sliding contact bearing · CPC title

• F04D29/10

  Shaft sealings · CPC title

• F01D25/166

  Sliding contact bearing (gas bearings F01D25/22) · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F04D29/0563

  Bearings cartridges · CPC title