Turbocharger and method

• US 9,739,238 B2
• Filed: 03/09/2015
• Issued: 08/22/2017
• Est. Priority Date: 03/09/2015
• Status: Active Grant

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Annati, Richard E., Williams, Thomas J.
• Primary Examiner(s): Trieu, Thai Ba
• Application Number:
  US14/641,660
• Publication Number:
  US 20160281644A1
• Time in Patent Office: 897 Days
• Field of Search: 606051, 606052, 606053, 417406-407, 384 99, 384475, 384535, 384585, 384906, 184 611
• CPC Class Codes: F01D 25/16 Arrangement of bearings; Supporting or mounting bearings in casings bearings per se F16C
• 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: F02M 26/04 with a single turbocharger
• CPC Class Codes: F04D 29/059 Roller bearings
• CPC Class Codes: F04D 29/4206 especially adapted for elastic fluid pumps
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F16C 19/184 in O-arrangement
• CPC Class Codes: F16C 2240/70 Diameters; Radii
• CPC Class Codes: F16C 2360/24 Turbochargers
• CPC Class Codes: F16C 33/586 outside the space between the races, e.g. end faces or bore of inner ring
• CPC Class Codes: F16C 33/588 Races of sheet metal
• CPC Class Codes: F16C 33/60 divided or split, e.g. comprising two juxtaposed rings
• CPC Class Codes: F16C 33/6651 in recesses or cavities provided in retainers, races or rolling elements
• CPC Class Codes: F16C 33/6659 Details of supply of the liquid to the bearing, e.g. passages or nozzles
• CPC Class Codes: F16C 33/767 integral with the race
• CPC Class Codes: F16C 33/80 Labyrinth sealings F16C33/761 takes precedence

Abstract

A turbocharger includes a turbine, a compressor, and a bearing housing forming a bearing bore. A bearing arrangement is disposed between a shaft interconnecting the turbine and compressor wheels, and the bearing housing. The bearing arrangement includes first and second bearings formed between an outer bearing race element disposed within the bearing bore an inner bearing race element disposed within the outer bearing race element and between the outer bearing race element and the shaft. The inner bearing race element includes a flared portion extending radially outwardly to provide torsional and bending rigidity to 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;

an outer race disposed within the bearing bore and including a first outer race end portion and a second outer race end portion; and

an inner race disposed within the outer race and between the outer race and the shaft, the inner race including a first inner race end portion and a second inner race end portion, the first inner race end portion being axially aligned with the first outer race end portion and the second inner race end portion being axially aligned with the second outer race end portion, wherein the inner race is formed by two components, a compressor-side cup and a turbine-side cup, wherein one of the turbine-side and compressor-side cups forms a ledge and a wall that accepts therein a free, annular face of the other cup;

a first bearing including a first plurality of rollers disposed between the first inner race end portion and the first outer race end portion;

a second bearing including a second plurality of rollers disposed between the second inner race end portion and the second outer race end portion,

wherein the inner race includes a flared portion disposed between the first inner race end portion and the second inner race end portion, the flared portion extending radially outwardly with respect to the first inner race end portion and the second inner race end portion to provide torsional and bending rigidity to the shaft, wherein the flared portion is flanked by two transition portions that reduce an inner diameter of the flared portion to match an outer diameter of the shaft, wherein each of the two transition portions has a smooth or chamfered profile,

wherein the shaft is connected to the inner race at the first and second inner race end portions, the shaft having a first shaft diameter adjacent the first and second inner race end portions, the shaft including a slender portion extending from the first inner race end portion to the second inner race end portion, the slender portion having a uniform second shaft diameter that is less than the first shaft diameter.

2. The turbocharger of claim 1, wherein the flared portion forms an increased inner diameter of the inner race.

3. The turbocharger of claim 1, wherein the increased inner diameter of the inner race overlaps in an axial direction with the slender portion of the shaft.

4. The turbocharger of claim 1, wherein the inner race engages the shaft at the first and second inner race end portions such that a closed cavity is formed between an inner surface of the flared portion and an outer surface of the shaft, the closed cavity being generally disposed against ingress of lubricating oil therein.

5. The turbocharger of claim 1, wherein the inner race, the outer race, and the respective first and second rollers are insertable together as an assembly into the bearing bore of the bearing housing around the shaft from one end, and are retained therein by a bearing retainer that is connected to the bearing housing.

6. A method for rotatably supporting a shaft within a bearing housing of a turbocharger, comprising:

forming a first roller bearing by engaging a first plurality of rollers with a first inner race end portion formed in an inner race and with a first outer race end portion formed in an outer race;

forming a second roller bearing by engaging a second plurality of rollers with a second inner race end portion formed in the inner race and with a second outer race end portion formed in the outer race;

engaging the outer race between a bearing bore formed in the bearing housing and the shaft extending through the bearing bore,

wherein the inner race engages the shaft at the first and second inner race end portions and includes a flared portion between the first and second inner race end portions such that the flared portion extends radially outwardly with respect to the first and second inner race end portions to provide torsional and bending rigidity to the shaft, wherein the flared portion is hollow and forms an increased inner diameter of the inner race, and

wherein the shaft is connected to the inner race at the first and second inner race end portions, the shaft having a first shaft diameter adjacent the first and second inner race end portions, the shaft including a slender portion extending from the first inner race end portion to the second inner race end portion, the slender portion having a uniform second shaft diameter that is less than the first shaft diameter.

7. The method of claim 6, wherein the increased inner diameter of the inner race overlaps in an axial direction with the slender portion of the shaft.

8. The method of claim 6, further comprising assembling the inner race using a compressor-side cup and a turbine-side cup, wherein one of the turbine-side and compressor-side cups forms a ledge and a wall that accepts therein a free, annular face of the other cup.

9. The method of claim 6, wherein the flared portion is flanked by two transition portions that reduce an inner diameter of the flared portion to match an outer diameter of the shaft.

10. The method of claim 9, wherein each of the two transition portions has a smooth or chamfered profile.

11. The method of claim 6, further comprising forming a closed cavity between an inner surface of the flared portion and an outer surface of the shaft, the closed cavity being generally disposed against ingress of lubricating oil therein.

12. The method of claim 6, wherein the inner race, the outer race, and the respective first and second rollers are insertable together as an assembly into the bearing bore of the bearing housing around the shaft from one end, and are retained therein by a bearing retainer that is connected to the bearing housing.

13. 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 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 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;

an outer race disposed within the bearing bore including a first outer race end portion and a second outer race end portion; and

an inner race disposed within the outer race and between the outer race and the shaft, the inner race including a first inner race end portion and a second inner race end portion, the first inner race end portion being axially aligned with the first outer race end portion and the second inner race end portion being axially aligned with the second outer race end portion;

a first bearing including a first plurality of rollers disposed between the first inner race end portion and the first outer race end portion;

a second bearing including a second plurality of rollers disposed between the second inner race end portion and the second outer race end portion,

wherein the inner race includes a flared portion disposed between the first inner race end portion and the second inner race end portion, the flared portion extending radially outwardly with respect to the first inner race end portion and the second inner race end portion to provide torsional and bending rigidity to the shaft,

wherein the shaft is connected to the inner race at the first and second inner race end portions, the shaft having a first shaft diameter adjacent the first and second end inner race end portions, the shaft further forming a slender portion extending from the first inner race end portion to the second end inner race end portions, the slender portion having a uniform second shaft diameter that is less than the first shaft diameter, and

wherein the increased inner diameter of the inner race overlaps in an axial direction with the slender portion of the shaft.