Swirl inducing bearing housing spacer and core

Patent metadata

Field	Value
Publication number	US-9970448-B2
Application number	US-201314439276-A
Country	US
Kind code	B2
Filing date	Nov 4, 2013
Priority date	Nov 12, 2012
Publication date	May 15, 2018
Grant date	May 15, 2018

Abstract

A turbocharger ( 10 ) having a bearing housing ( 14 ) between a turbine housing and a compressor housing with a shaped core ( 16 ) forming an internal oil drain cavity ( 20 ) adjacent to a spacer ( 24 ) shaped to induce swirling for oil defoaming. A depression ( 18 ) in an internal core wall of the bearing housing ( 14 ) forms the oil drain cavity ( 20 ) with each end ( 22 ) of the depression ( 18 ) corresponding to a distal end ( 30 ) of the spacer ( 24 ). The spacer ( 24 ) is preferably substantially tubular with a row of oil-flow apertures ( 32 ) aligned on each outer span ( 34 ) of a recessed center portion ( 28 ) to induce swirling.

First claim

What is claimed is:

1. A turbocharger ( 10 ) comprising:
a bearing housing ( 14 ) with a core ( 16 ) having a depression ( 18 ) wherein diameters at ends ( 22 ) of the depression ( 18 ) are smaller than a diameter between the ends ( 22 ) of the depression ( 18 ) thereby forming an oil drain cavity ( 20 ) adjacent to a spacer ( 24 ) shaped to induce swirling for oil defoaming, wherein a diameter of a center portion ( 28 ) of the spacer ( 24 ) between the ends ( 22 ) of the depression ( 18 ) is smaller than diameters of distal ends ( 30 ) of the spacer ( 24 ).

2. The turbocharger ( 10 ) of claim 1 wherein the depression ( 18 ) is U-shaped in the bearing housing ( 14 ) adjacent to the center portion ( 28 ) of the spacer ( 24 ), and the ends ( 22 ) of the depression ( 18 ) correspond to the distal ends ( 30 ) of the spacer ( 24 ).

3. The turbocharger ( 10 ) of claim 1 wherein the spacer ( 24 ) is substantially tubular with the center portion ( 28 ) being inwardly recessed and having a row of oil-flow apertures ( 32 ) aligned on each outer span ( 34 ) of the center portion ( 28 ), wherein the rows of oil-flow apertures ( 32 ) are aligned with the ends ( 22 ) of the depression ( 18 ).

4. The turbocharger ( 10 ) of claim 3 wherein each row of oil-flow apertures ( 32 ) includes at least eight apertures.

5. The turbocharger ( 10 ) of claim 3 wherein the distal ends ( 30 ) of the spacer ( 24 ) are cylindrical and aligned with corresponding round wall portions of the core ( 16 ) so that oil flows toward the center portion ( 28 ).

6. The turbocharger ( 10 ) of claim 1 wherein the oil drain cavity ( 20 ) is above an oil drain ( 26 ) for return of oil to an engine crankcase.

7. A turbocharger ( 10 ) comprising:
a bearing housing ( 14 ) with a core ( 16 ) having a depression ( 18 ) in the bearing housing ( 14 ) wherein diameters at opposite ends ( 22 ) of the depression ( 18 ) are smaller than a diameter between the opposite ends ( 22 ) of the depression thereby forming an oil drain cavity ( 20 ) on each side of a substantially tubular spacer ( 24 ),
wherein the substantially tubular spacer ( 24 ) includes an inwardly recessed center portion ( 28 ) positioned between two rows of oil-flow apertures ( 32 ) aligned on each outer span ( 34 ) of the inwardly recessed center portion ( 28 ) to induce swirling for oil defoaming, wherein a diameter of the inwardly recessed center portion ( 28 ) is smaller than diameters of the outer spans ( 34 ), and wherein the distal ends ( 30 ) of the substantially tubular spacer ( 24 ) align with the opposite ends ( 22 ) of the depressions ( 18 ) in the bearing housing ( 14 ).

Assignees

• Borgwarner Inc

Inventors

• Bucking Michael

Classifications

• F16C17/26

  Systems consisting of a plurality of sliding-contact bearings · CPC title

• F04D29/0563

  Bearings cartridges · CPC title

• F16C2360/24

  Turbochargers · 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

• F04D29/056 Primary

  Bearings · CPC title