Turbocharger bearing housing with integrated heat shield
A system and method is provided in which a turbocharger includes a heat shield wall that is formed together with the bearing housing as a unitary structure. The wall can extend from a main body portion of the bearing housing in a generally radially outward direction. The wall can be spaced from the main body and attached by a plurality of ribs such that chambers are defined therebetween. A circumferential passage can extend through the bearing housing to permit fluid communication between the chambers and outside of the bearing housing. In this way, a fluid outlet from the chambers is provided. As a result of such an arrangement, the need for a separate heat shield is eliminated, which can facilitate the assembly process and special attachment methods associated with a separate heat shield.
1. A bearing housing ( 52 ) for a turbocharger comprising:
a main body ( 53 );
a radially outwardly extending heat shield wall ( 50 ), the heat shield wall ( 50 ) and the main body ( 53 ) being formed together as a unitary structure and connected by a plurality of ribs ( 70 ), the heat shield wall ( 50 ) being spaced from the main body ( 53 ) such that a plurality of chambers ( 72 ) are formed, each chamber ( 72 ) being at least partly defined by the heat shield wall ( 50 ), the main body ( 53 ) and neighboring pairs of ribs ( 70 ); and
at least one passage ( 86 ) extending through the bearing housing ( 52 ) to permit fluid communication between the plurality of chambers ( 72 ) and outside of the bearing housing ( 52 ), whereby an exit from the plurality of chambers ( 72 ) is provided.
2. The bearing housing of claim 1 , wherein the heat shield wall ( 50 ) is connected to the main body ( 53 ) exclusively by the plurality of ribs ( 70 ).
3. The bearing housing of claim 1 , wherein the plurality of ribs ( 70 ) are substantially equally spaced.
4. The bearing housing of claim 1 , wherein the at least one passage ( 86 ) is a circumferential slot.
5. The bearing housing of claim 1 , wherein the at least one passage ( 86 ) extends substantially perpendicular to an axis ( 54 ) of a shaft bore ( 55 ) in the bearing housing ( 52 ).
6. The bearing housing of claim 1 , wherein the at least one passage ( 86 ) extends substantially parallel to an axis ( 54 ) of a shaft bore ( 55 ) in the bearing housing ( 52 ).
7. The bearing housing of claim 1 , wherein the heat shield wall ( 50 ) has an associated thickness, wherein the thickness of the heat shield wall ( 50 ) increases from a radially inner end region ( 62 ) to a radially outer end region ( 64 ) thereof.
8. The bearing housing of claim 1 , wherein the at least one passage ( 86 ) is formed in a radially inner end region ( 62 ) of the heat shield wall ( 50 ).
9. A turbocharger system comprising:
a bearing housing ( 52 ) having a main body ( 53 ) with a shaft bore ( 55 ) for receiving a rotatable shaft therein, the shaft bore ( 55 ) having an associated longitudinal axis ( 54 ), the bearing housing ( 52 ) further including a radially outwardly extending heat shield wall ( 50 ), the heat shield wall ( 50 ) and the main body ( 53 ) being formed together as a unitary structure and connected by a plurality of ribs ( 70 ), the heat shield wall ( 50 ) being spaced from the main body ( 53 ) such that a plurality of chambers ( 72 ) are formed, each chamber ( 72 ) being at least partly defined by the heat shield wall ( 50 ), the main body ( 53 ) and neighboring pairs of ribs ( 70 ); and
a shaft ( 56 ), at least a portion of the shaft ( 56 ) being rotatably received within the shaft bore ( 55 );
a turbine wheel ( 84 ) being provided at one end of the shaft ( 56 ), the turbine wheel ( 84 ) including a backface ( 82 ), the heat shield wall ( 50 ) being disposed between the main body ( 53 ) and the backface ( 82 ) of the turbine wheel ( 84 ) such that a volume ( 80 ) is at least partially defined between the heat shield wall ( 50 ) and the backface ( 82 ); and
at least one passage ( 86 ) extending through the bearing housing ( 52 ) to permit fluid communication between the plurality of chambers ( 72 ) and the volume ( 80 ), whereby an exit from the plurality of chambers ( 72 ) is provided.
10. The turbocharger system of claim 9 , wherein the heat shield wall ( 50 ) is connected to the main body ( 53 ) exclusively by the plurality of ribs ( 70 ).
11. The turbocharger system of claim 9 , wherein the plurality of ribs ( 70 ) are substantially equally spaced.
12. The turbocharger system of claim 9 , wherein the at least one passage ( 86 ) is a circumferential slot.
13. The turbocharger system of claim 9 , wherein an entry to the plurality of chambers ( 72 ) is defined between an outer peripheral surface ( 66 ) of the heat shield wall ( 50 ) and a portion of a stationary structure of a turbine housing ( 18 ).
14. A method of forming a bearing housing for a turbocharger comprising:
casting a bearing housing ( 52 ) having a main body ( 53 ) and a radially outwardly extending heat shield wall ( 50 ), whereby the main body ( 53 ) and the heat shield wall ( 50 ) are a unitary structure and connected by a plurality of ribs ( 70 ), the heat shield wall ( 50 ) being spaced from the main body ( 53 ) such that a plurality of chambers ( 72 ) are formed, each chamber ( 72 ) being at least partly defined by the heat shield wall ( 50 ), the main body ( 53 ), and neighboring pairs of ribs ( 70 ).
15. The method of claim 14 , further including:
forming at least one passage ( 86 ) in the bearing housing ( 52 ) to permit fluid communication between the plurality of chambers ( 72 ) and outside of the bearing housing ( 52 ), whereby an exit from the plurality of chambers ( 72 ) is provided.