Turbocharger bearing assembly

• US 4,902,144 A
• Filed: 05/02/1989
• Issued: 02/20/1990
• Est. Priority Date: 05/02/1989
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Alliedsignal Inc.
• Inventors: Thoren, Dennis F.
• Primary Examiner(s): Footland, Lenard A.
• Application Number:
  US07/345,990
• Time in Patent Office: 294 Days
• Field of Search: 384/398, 384/99, 384/901, 384/287, 384/399, 384/369, 384/551
• US Class Current: 384/398
• CPC Class Codes: F01D 25/166 Sliding contact bearing gas bearings F01D25/22
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F16C 17/02 for radial load only
• CPC Class Codes: F16C 17/18 with floating brasses or brushing, rotatable at a reduced speed F16C17/03, F16C17/06 take precedence
• CPC Class Codes: F16C 17/26 Systems consisting of a plurality of sliding-contact bearings
• CPC Class Codes: F16C 2360/24 Turbochargers in general F02C6/12
• CPC Class Codes: Y10S 384/901 Floating bushing

Abstract

An improved bearing assembly is provided for axially retaining journal bearings in a turbocharger. The turbocharger includes a center housing having an elongated bearing bore for receiving an axially spaced pair of journal bearings which in turn support a rotatable turbocharger shaft. Lubricating oil is supplied through the center housing for passage to the shaft-bearing interface through radially open oil flow ports formed in the journal bearings. A bearing spacer is interposed axially between the journal bearings such that the opposite ends of the bearing spacer define a pair of thrust surfaces for engaging and locating the axially inboard faces of the journal bearings. Additional thrust surfaces are formed on thrust members carried by the turbocharger shaft to engage and locate the axially outboard faces of the journal bearings. The outer diameters of these thrust surfaces are less than the outer diameter of the journal bearings to promote substantially unimpeded, axially bidirectional oil flow over and about the journal bearings.

Claims

1. A turbocharger bearing assembly for rotatably supporting a turbocharger shaft within a bearing bore formed in a turbocharger center housing, said assembly comprising:

a pair of rotationally floating journal bearings within said bearing bore and rotationally supporting said shaft;

a generally cylindrical, rotationally floating bearing spacer carried about said shaft and axially interposed between said journal bearings, said spacer having opposite ends defining a pair of axially outwardly presented inboard thrust surfaces for engaging axially inboard faces of said journal bearings to maintain said journal bearings in precision axial spaced relation; and

a pair of axially inwardly presented outboard thrust surfaces defined by a pair of thrust members carried with said shaft for engaging axially outboard faces of said journal bearings;

said inboard and outboard thrust surfaces having outer diameters substantially less than the outer diameters of said journal bearings.

2. The turbocharger bearing assembly of claim 1 wherein said spacer has an inner diameter substantially greater than the outer diameter of said shaft.

3. The turbocharger bearing assembly of claim 1 wherein said spacer has an effective outer diameter substantially less than the diametric size of said bearing bore, said spacer further including pilot means radiating outwardly from said spacer outer diameter for piloting said spacer within said bearing bore.

4. The turbocharger bearing assembly of claim 1 wherein said journal bearings each include a generally axially centered, circumferentially spaced array of radially open oil flow ports, and further including oil flow means for supply of oil flow through said center housing to said journal bearings at generally axially centered positions with respect to said journal bearings, wherein said inboard and outboard thrust surfaces accommodate substantially unimpeded bidirectional oil flow about said journal bearings.

5. The turbocharger bearing assembly of claim 4 wherein said spacer has at least one central outlet opening formed therein to permit radial escape of oil from the interior of said spacer.

6. The turbocharger bearing assembly of claim 1 further including means for fixing the axial spacing between said outboard thrust surfaces to provide at least some axial float of said journal bearings and said spacer disposed in coaxial stacked relation between said outboard thrust surfaces.

7. The turbocharger bearing assembly of claim 1 wherein said spacer is formed from a plastic material.

8. A turbocharger bearing assembly for rotatably supporting a turbocharger shaft within a bearing bore formed in a turbocharger center housing, said assembly comprising:

a pair of rotationally floating journal bearings within said bearing bore and rotationally supporting said shaft;

a generally cylindrical bearing spacer carried about said shaft for rotational floating within said bearing bore and disposed axially between said journal bearings, said spacer having an inner diameter surface and an outer diameter surface disposed in substantial clearance with respect to said shaft and bearing bore, respectively, and pilot means radiating outwardly from said outer diameter surface for rotationally piloting said spacer within said bearing bore;

said spacer having opposite ends defining a pair of axially outwardly presented inboard thrust surfaces for engaging axially inboard faces of said journal bearings to maintain said journal bearings in precision axial spaced relation, said inboard thrust surfaces having an effective outer diameter substantially less than the outer diameters of said journal bearings;

a pair of thrust members carried by said shaft and defining a pair of axially inwardly presented outboard thrust surfaces for engaging axially outboard faces of said journal bearings, said outboard thrust surfaces having an outer diameter substantially less than the outer diameters of said journal bearings;

means for fixing the axial spacing between said outboard thrust surfaces to provide at least some axial float for said journal bearings and said spacer sleeve; and

oil flow means for supplying lubricating oil to said journal bearings at generally axially centered positions with respect to said journal bearings, said journal bearings including circumferentially spaced arrays of radially open oil flow ports to permit oil flow to the interface between said bearings and the shaft;

said spacer further defining a central outlet opening to permit radial escape of oil to the exterior of said spacer.

9. The turbocharger bearing assembly of claim 8 wherein said bearing bore has a substantially uniform diametric size extending the length thereof.

10. The turbocharger bearing assembly of claim 8 wherein said pilot means comprises a circumferentially spaced array of arcuately narrow pilot tabs formed generally adjacent each end of said spacer.

11. The turbocharger bearing assembly of claim 8 wherein said thrust members respectively comprise a stepped shoulder on said shaft and a thrust bearing unit mounted on said shaft.