Turbocharger purge seal including axisymmetric supply cavity

Patent metadata

Field	Value
Publication number	US-10240610-B2
Application number	US-201414905452-A
Country	US
Kind code	B2
Filing date	Jul 18, 2014
Priority date	Jul 26, 2013
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

A turbocharger rotating assembly (125) includes a shaft (20) rotatably supported in a bearing housing (123) via bearings (26, 128), a compressor impeller (18) mounted on the shaft (20), and an oil flinger (122) disposed on the shaft (20) between the bearings (26, 128) and the compressor impeller (18). The turbocharger (100) further includes an insert (134) disposed in the shaft-receiving axial bore (120) so as to surround the oil flinger (122), and a purge seal (160) operatively positioned in an interface (131) between the insert (134) and the oil flinger (122), whereby the purge seal (160) is configured to minimize oil passage from the bearing housing (123) into the interface (131). An annular cavity (150) encircles the radially outward-facing surface (138) of the insert (134), the cavity (150) forming a portion of a fluid path configured to deliver pressurized fluid to the interface (131).

First claim

What is claimed is:

1. A sealing system ( 110 ) for a turbocharger ( 100 ) that comprises
a bearing housing ( 123 ) including an axial bore ( 120 );
a rotating assembly ( 125 ) including
a shaft ( 20 ) having axis of rotation ( 21 ), the shaft ( 20 ) rotatably supported in the axial bore ( 120 ) via bearings ( 26 , 128 ),
a compressor impeller ( 18 ) mounted on the shaft ( 20 ),
an oil flinger ( 122 ) disposed on the shaft ( 20 ) between the bearings ( 26 , 128 ) and the compressor impeller ( 18 ); and

a stationary insert ( 134 ) disposed in the axial bore ( 120 ) so as to surround the oil flinger ( 122 ), the stationary insert ( 134 ) defining a radially outward-facing surface ( 138 );

the sealing system ( 110 ) including
a purge seal ( 160 ) operatively positioned in an interface ( 131 ) between the stationary insert ( 134 ) and the oil flinger ( 122 ), the purge seal ( 160 ) configured to introduce pressurized fluid into the interface ( 131 ), and including an annular cavity ( 150 ) encircling the radially outward-facing surface ( 138 ) of the stationary insert ( 134 ), the cavity ( 150 ) forming a portion of a fluid path configured to deliver the pressurized fluid to the interface ( 131 ),
wherein the stationary insert ( 134 ) includes at least one radial bore ( 139 ) that opens to both the cavity ( 150 ) and the interface ( 131 ), and forms another portion of the fluid path.

2. The sealing system ( 110 ) of claim 1 comprising a first piston ring ( 32 ) and a second piston ring ( 32 ), the first and second piston rings ( 32 ) disposed between a radially-outward facing surface of the oil flinger ( 122 ) and the stationary insert ( 134 ),
wherein the radial bore ( 139 ) communicates with the interface ( 131 ) at a location between the first piston ring ( 32 ) and the second piston ring ( 32 ).

3. The sealing system ( 110 ) of claim 1 , wherein the stationary insert ( 134 ) includes a radially-extending sealing flange ( 140 ), and the cavity ( 150 ) is defined between the bearing housing ( 123 ), the radially outward-facing surface ( 138 ) of the stationary insert ( 134 ), and the sealing flange ( 140 ).

4. The sealing system ( 110 ) of claim 3 , wherein the sealing flange ( 140 ) abuts an axial surface (S 2 ) of the bearing housing ( 123 ).

5. The sealing system ( 110 ) of claim 4 , wherein the sealing flange ( 140 ) is retained in position relative to the bearing housing ( 123 ) by a snap ring ( 118 ).

6. The sealing system ( 110 ) of claim 1 , wherein the position of the stationary insert ( 134 ) relative to the bearing housing ( 123 ) is maintained by a snap ring ( 118 ) disposed between the stationary insert ( 134 ) and a portion of the bearing housing ( 123 ).

7. The sealing system ( 110 ) of claim 1 , including a supply passageway ( 154 ) in fluid communication with the cavity ( 150 ), the supply passageway ( 154 ) forming another portion of the fluid path.

8. The sealing system ( 110 ) of claim 1 , comprising an O-ring ( 116 ) disposed in a groove ( 142 ) on the radially outward-facing surface ( 138 ) of the stationary insert ( 134 ), the O-ring ( 116 ) providing a seal between the radially outward-facing surface ( 138 ) of the stationary insert ( 134 ) and a radially-inward facing surface ( 123 a ) of the bearing housing ( 123 ).

9. A turbocharger ( 100 ), comprising
a bearing housing ( 123 ), the bearing housing ( 123 ) including an axial bore ( 120 );
a turbine stage ( 12 ) connected to one end of the bearing housing ( 123 );
a compressor stage ( 14 ) connected to an opposed end of the bearing housing ( 123 );
a rotating assembly ( 125 ) including
a shaft ( 20 ) having axis of rotation ( 21 ), the shaft ( 20 ) rotatably supported in the axial bore ( 120 ) via bearings ( 26 , 128 ),
a compressor impeller ( 18 ) mounted on the shaft ( 20 ), and
an oil flinger ( 122 ) disposed on the shaft ( 20 ) between the bearings ( 26 , 128 ) and the compressor impeller ( 18 );

a stationary insert ( 134 ) disposed in the axial bore ( 120 ) so as to surround the oil flinger ( 122 ), the stationary insert ( 134 ) defining a radially outward-facing surface ( 138 );
a purge seal ( 160 ) operatively positioned in an interface ( 131 ) between the stationary insert ( 134 ) and the oil flinger ( 122 ), the purge seal ( 160 ) configured to introduce pressurized fluid into the interface ( 131 ), and including an annular cavity ( 150 ) encircling the radially outward-facing surface ( 138 ) of the stationary insert ( 134 ), the cavity ( 150 ) forming a portion of a fluid path configured to deliver the pressurized fluid to the purge seal ( 160 ),
wherein the stationary insert ( 134 ) includes at least one radial bore ( 139 ) that opens to both the cavity ( 150 ) and the interface ( 131 ), and forms another portion of the fluid path.

10. The turbocharger ( 100 ) of claim 9 , wherein the stationary insert ( 134 ) includes a radially-extending sealing flange ( 140 ), and the cavity ( 150 ) is defined between the bearing housing ( 123 ), the radially outward-facing surface ( 138 ) of the stationary insert ( 134 ), and the sealing flange ( 140 ).

11. The turbocharger ( 100 ) of claim 9 comprising a first piston ring ( 32 ) and a second piston ring ( 32 ), the first and second piston rings ( 32 ) disposed between a radially outward-facing surface of the oil flinger ( 122 ) and the stationary insert ( 134 ),
wherein the radial bore ( 139 ) communicates with the interface ( 131 ) at a location between the first piston ring ( 32 ) and the second piston ring ( 32 ).

12. The turbocharger ( 100 ) of claim 9 , including a supply passageway ( 154 ) in fluid communication with the cavity ( 150 ), the supply passageway ( 154 ) forming another portion of the fluid path.

13. The turbocharger ( 100 ) of claim 9 , wherein the position of the stationary insert ( 134 ) relative to the bearing housing ( 123 ) is maintained by a snap ring ( 118 ) disposed between the insert ( 134 ) and a portion of the bearing housing ( 123 ).

Assignees

• Borgwarner Inc

Inventors

• Kelly Allan D
• Ellwood E Perry
• Ashton Zachary
• Race Robert T

Classifications

• F01D25/183

  Sealing means · CPC title

• F02B33/32

  Engines with pumps other than of reciprocating-piston type (with crankcase pumps F02B33/02) · CPC title

• F01D11/04

  using sealing fluid, e.g. steam · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F04D25/024

  the driving means being assisted by a power recovery turbine · CPC title