Turbocharger with oil containment arrangement

• US 9,822,700 B2
• Filed: 03/09/2015
• Issued: 11/21/2017
• Est. Priority Date: 03/09/2015
• Status: Expired due to Fees

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Annati, Richard E., Harnadek, David
• Primary Examiner(s): Nguyen, Ngoc T
• Application Number:
  US14/642,059
• Publication Number:
  US 20160265426A1
• Time in Patent Office: 988 Days
• Field of Search: 606053
• CPC Class Codes: F01D 25/005 Selecting particular materials
• CPC Class Codes: F01D 25/16 Arrangement of bearings; Supporting or mounting bearings in casings bearings per se F16C
• CPC Class Codes: F01D 25/183 Sealing means
• CPC Class Codes: F01D 5/025 Fixing blade carrying members on shafts attachment of a member on a shaft in general F16D1/06; for non-positive displacement pumps F04D29/00
• CPC Class Codes: F02B 37/00 Engines characterised by provision of pumps driven at least for part of the time by exhaust
• CPC Class Codes: F02B 39/14 Lubrication of pumps; Safety measures therefor
• CPC Class Codes: F02M 35/10157 Supercharged engines
• CPC Class Codes: F04D 25/024 the driving means being assisted by a power recovery turbine
• CPC Class Codes: F04D 29/059 Roller bearings
• CPC Class Codes: F04D 29/102 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/266 mounting compressor rotors on shafts
• CPC Class Codes: F04D 29/624 especially adapted for elastic fluid pumps
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2240/54 Radial bearings
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: F16C 19/184 in O-arrangement
• CPC Class Codes: F16C 2360/24 Turbochargers
• CPC Class Codes: F16C 33/581 integral with other parts, e.g. with housings or machine elements such as shafts or gear wheels
• CPC Class Codes: F16C 33/6685 Details of collecting or draining, e.g. returning the liquid to a sump
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A turbocharger is provided including a turbine, a compressor and a bearing housing. A shaft is rotatably disposed within the bearing housing and extends into the turbine and the compressor. A bearing arrangement is disposed between the shaft and the bearing. The bearing arrangement includes a roller bearing formed between an outer bearing race element disposed in the bearing bore, and an inner bearing race element disposed in the outer bearing race element. A bearing retainer connected between the bearing housing and the compressor. An end portion of the bearing inner race element includes an integral oil slinger comprising a radially outward extending portion that slopes away from the shaft.

Claims

1. A turbocharger, comprising:

a turbine that includes a turbine wheel;

a compressor that includes a compressor wheel;

a bearing housing disposed and connected between the turbine and the compressor, the bearing housing forming a bearing bore therethrough;

a shaft rotatably disposed within the bearing housing and extending into the turbine and the compressor, wherein the turbine wheel is connected to one end of the shaft and wherein the compressor wheel is connected to an opposite end of the shaft such that the turbine wheel is rotatably disposed in the turbine and the compressor wheel is rotatably disposed in the compressor;

a bearing arrangement disposed between the shaft and the bearing housing, the bearing arrangement including a roller bearing formed between an outer bearing race disposed in the bearing bore, and an inner bearing race disposed in the outer bearing race, wherein the inner bearing race is arranged to rotate with the shaft, and wherein an end portion of the bearing inner race includes an integral oil slinger comprising a radially outward extending portion that slopes away from the shaft; and

a bearing retainer connected between the bearing housing and the compressor, the bearing retainer forming an inner bore through which the shaft extends, and a ring seal disposed to sealably engage the inner bearing race and the inner bore of the bearing retainer, wherein a tortuous path is provided between an oil collection gallery of the bearing housing and the ring seal.

2. The turbocharger of claim 1 wherein the ring seal is arranged in a U-shaped channel defined by a shoulder of the compressor wheel and an open channel in the inner bearing race.

3. The turbocharger of claim 1 wherein the tortuous path is defined along an interface between the bearing retainer and the inner bearing race to discourage oil flow towards the ring seal.

4. The turbocharger of claim 3 wherein the bearing retainer forms an inwardly facing cylindrical wall around the inner bore, and wherein the tortuous path is defined between the oil slinger and the radially outward extending portion, which are axially aligned.

5. The turbocharger of claim 1 wherein the shaft is connected to the inner bearing race at end portions, the end portions having a first diameter, the shaft further forming a slender portion between the end portions, the slender portion having a second diameter that is less than the first diameter.

6. The turbocharger of claim 5 wherein the increased inner diameter of the inner bearing race overlaps in an axial direction with the slender portion of the shaft.

7. The turbocharger of claim 1 wherein the inner bearing race is formed by two components, an outboard cup and an inboard cup.

8. The turbocharger of claim 1 wherein the bearing retainer includes an outlet passage communicating with a lubrication cavity and a drip lip adjacent the outlet passage.

9. An internal combustion engine having a plurality of combustion chambers formed in a cylinder block, an intake manifold disposed to provide air or a mixture of air with exhaust gas to the combustion chambers, and an exhaust manifold disposed to receive exhaust gas from the combustion chambers, the engine further comprising:

a turbine that includes a turbine housing surrounding a turbine wheel, the turbine housing being fluidly connected to the exhaust manifold and disposed to receive exhaust gas therefrom to drive the turbine wheel;

a compressor that includes a compressor housing that surrounds a compressor wheel, the compressor housing being fluidly connected to the intake manifold and disposed to provide air thereto;

a bearing housing disposed and connected between the turbine and the compressor, the bearing housing forming a bearing bore therethrough;

a shaft rotatably disposed within the bearing housing and extending into the turbine and the compressor, wherein the turbine wheel is connected to one end of the shaft and wherein the compressor wheel is connected to an opposite end of the shaft such that the turbine wheel is rotatably disposed in the turbine and the compressor wheel is rotatably disposed in the compressor;

a bearing arrangement disposed between the shaft and the bearing housing, the bearing arrangement including a roller bearing formed between an outer bearing race disposed in the bearing bore, and an inner bearing race disposed in the outer bearing race, wherein the inner bearing race is arranged to rotate with the shaft, and wherein an end portion of the inner bearing race includes an integral oil slinger comprising a radially outward extending portion that slopes away from the shaft; and

a bearing retainer connected between the bearing housing and the compressor, the bearing retainer forming an inner bore through which the shaft extends, and the ring seal disposed to sealably engage the inner bearing race and the inner bore of the bearing retainer, wherein a tortuous path is provided between an oil collection gallery of the bearing housing and the ring seal.

10. A turbocharger, comprising:

a turbine that includes a turbine housing surrounding a turbine wheel;

a compressor that includes a compressor housing that surrounds a compressor wheel;

a bearing housing disposed and connected between the turbine and the compressor, the bearing housing forming a bearing bore therethrough that accommodates a shaft interconnecting the turbine wheel and the compressor wheel to transfer power therebetween;

wherein the shaft is rotatably mounted within the bearing housing and extends into the turbine and the compressor such that the turbine wheel is connected to one end of the shaft and the compressor wheel is connected to an opposite end of the shaft;

a bearing arrangement disposed between the shaft and the bearing housing, the bearing arrangement including first and second bearings, each of the first and second bearings formed by a respective first and second plurality of rollers engaged between a respective first and second inner race and a respective first and second outer race;

an outer bearing race disposed within the bearing bore and forming the respective first and second outer races;

an inner bearing race disposed within the outer bearing race and between the outer bearing race and the shaft, the inner bearing race forming the respective first and second inner races such that the respective first inner race is axially aligned with the respective first outer race, and the respective second inner race is axially aligned with the respective second outer race, wherein the inner bearing race is arranged to rotate with the shaft, and wherein an end portion of the bearing inner race includes an integral oil slinger comprising a radially outward extending portion that slopes away from the shaft; and

a bearing retainer connected between the bearing housing and the compressor, the bearing retainer forming an inner bore through which the shaft extends, and a ring seal disposed to sealably engage the inner bearing race and the inner bore of the bearing retainer, wherein a tortuous path is provided between an oil collection gallery of the bearing housing and the ring seal.

11. The turbocharger of claim 10 wherein the ring seal is arranged in a U-shaped channel defined by a shoulder of the compressor wheel and an open channel in the inner bearing race.

12. The turbocharger of claim 10 wherein the tortuous path is defined along an interface between the bearing retainer and the inner bearing race to discourage oil flow towards the ring seal.

13. The turbocharger of claim 12 wherein the bearing retainer forms an inwardly facing cylindrical wall around the inner bore, and wherein the tortuous path is defined between the oil slinger and the radially outward extending portion, which are axially aligned.

14. The turbocharger of claim 10 wherein the bearing retainer includes an outlet passage communicating with a lubrication cavity and a drip lip adjacent the outlet passage.