Turbocharger bearing housing oil groove

Patent metadata

Field	Value
Publication number	US-9494189-B2
Application number	US-201414503528-A
Country	US
Kind code	B2
Filing date	Oct 1, 2014
Priority date	Apr 4, 2014
Publication date	Nov 15, 2016
Grant date	Nov 15, 2016

Abstract

A turbocharger for an internal combustion engine includes a bearing housing and a bearing bore defined by the bearing housing. The bearing bore has an annular bearing groove configured to receive a fluid. A journal bearing is disposed within the bore such that the annular bearing groove encircles the journal bearing and feeds the fluid thereto. The turbocharger also includes a rotating assembly having a shaft with a turbine wheel and a compressor wheel. The shaft has a longitudinal axis and is supported by the journal bearing for rotation within the bore about the axis. The annular bearing groove is characterized by a trapezoidal shape in a cross-sectional view of the bearing bore taken along and through the longitudinal axis. The trapezoidal shape is configured to generate Taylor vortices in the fluid for capturing debris carried by the fluid and keeping the debris from being fed to the journal bearing.

First claim

The invention claimed is:

1. An internal combustion engine comprising:
an engine block defining a combustion chamber configured to receive an air-fuel mixture for combustion therein and configured to exhaust post-combustion gasses therefrom; and
a turbocharger configured to receive an airflow from an ambient and the post-combustion gasses from the combustion chamber, the turbocharger including:
a bearing housing;
a bearing bore defined by the bearing housing and having an annular bearing groove configured to receive a fluid;
a journal bearing disposed within the bearing bore such that the annular bearing groove encircles the journal bearing and feeds the fluid thereto; and
a rotating assembly having a shaft with a turbine wheel configured to be driven by the post-combustion gasses and a compressor wheel configured to pressurize the airflow for delivery to the combustion chamber;
wherein:
the journal bearing includes a first surface defined by an inner diameter, a second surface defined by an outer diameter, and a passage that connects the first and second surfaces;
the shaft has a longitudinal axis and is supported by the journal bearing for rotation within the bearing bore about the longitudinal axis;
the annular bearing groove is characterized by a trapezoidal shape in a cross-sectional view of the bearing bore taken along and through the longitudinal axis and positioned to align with and feed the fluid through the passage; and
the trapezoidal shape is configured to generate Taylor vortices in the fluid for capturing debris carried by the fluid and keeping the debris from being fed to the journal bearing.

2. The engine of claim 1 , wherein the journal bearing is configured as a fully-floating bearing such that the fluid fed thereto forms a first fluid film between the bearing bore and the journal bearing and a second fluid film between the journal bearing and the shaft.

3. The engine of claim 2 , further comprising a fluid pump configured to pressurize the fluid, wherein the pressurized fluid is directed to the annular bearing groove to lubricate the journal bearing and generate the first and second fluid films.

4. The engine of claim 3 , wherein the bearing bore includes a wedge groove incorporated into the annular bearing groove and configured to use gravity to trap the debris when the fluid pump stops pressurizing the fluid.

5. The engine of claim 1 , wherein the passage includes a plurality of passages and the annular bearing groove is positioned to align with each of the plurality of passages and feed the fluid through the plurality of passages.

6. The engine of claim 1 , wherein the journal bearing is a plurality of journal bearings and the annular bearing groove is a plurality of annular bearing grooves, and wherein each annular bearing groove encircles a respective journal bearing.

7. The engine of claim 6 , wherein the journal bearing is a brass bushing.

8. The engine of claim 7 , wherein the annular bearing groove is one of machined and cast into the bearing housing.

9. A turbocharger for an internal combustion engine having a combustion chamber, the turbocharger comprising:
a bearing housing;
a bearing bore defined by the bearing housing and having an annular bearing groove configured to receive a fluid;
a journal bearing disposed within the bearing bore such that the annular bearing groove encircles the journal bearing and feeds the fluid thereto; and
a rotating assembly having a shaft with a turbine wheel configured to be driven by post-combustion gasses emitted by the combustion chamber and a compressor wheel configured to pressurize the airflow for delivery to the combustion chamber;
wherein:
the journal bearing includes a first surface defined by an inner diameter, a second surface defined by an outer diameter, and a passage that connects the first and second surfaces;
the shaft has a longitudinal axis and is supported by the journal bearing for rotation within the bearing bore about the longitudinal axis;
the annular bearing groove is characterized by a trapezoidal shape in a cross-sectional view of the bearing bore taken along and through the longitudinal axis and positioned to align with and feed the fluid through the passage; and
the trapezoidal shape is configured to generate Taylor vortices in the fluid for capturing debris carried by the fluid and keeping the debris from being fed to the journal bearing.

10. The turbocharger of claim 9 , wherein the journal bearing is configured as a fully-floating bearing such that the fluid fed thereto forms a first fluid film between the bearing bore and the journal bearing and a second fluid film between the journal bearing and the shaft.

11. The turbocharger of claim 10 , wherein the engine includes a fluid pump configured to pressurize the fluid, and wherein the pressurized fluid is directed to the annular bearing groove to lubricate the journal bearing and generate the first and second fluid films.

12. The turbocharger of claim 11 , wherein the bearing bore includes a wedge groove incorporated into the annular bearing groove and configured to use gravity to trap the debris when the fluid pump stops pressurizing the fluid.

13. The turbocharger of claim 9 , wherein the passage includes a plurality of passages and the annular bearing groove is positioned to align with each of the plurality of passages and feed the fluid through the plurality of passages.

14. The turbocharger of claim 9 , wherein the journal bearing is a plurality of journal bearings and the annular bearing groove is a plurality of annular bearing grooves, and wherein each annular bearing groove encircles a respective journal bearing.

15. The turbocharger of claim 14 , wherein the journal bearing is a brass bushing.

16. The turbocharger of claim 15 , wherein the annular bearing groove is one of machined and cast into the bearing housing.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Begin Louis P
• Deng Dingfeng
• Wu Ran
• Shi Fanghui

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F16C2240/42

  Groove sizes · CPC title

• F01D25/18

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• F04D29/057

  hydrostatic; hydrodynamic · CPC title

• F05D2260/607

  Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles · CPC title