Locating mechanism for turbocharger bearing
An exemplary semi-floating bearing for a turbocharger has a central axis defining a cylindrical coordinate system with an axial direction, a radial direction and an angular direction; a turbine end; a compressor end; journal surfaces between the turbine end and the compressor end, the surfaces configured to support a turbocharger shaft; and an opening disposed between the turbine end and the compressor end, the opening having a radial dimension that exceeds an axial dimension to, upon receipt of a locating pin, provide for movement of the bearing in the angular direction about its central axis and to provide for lesser movement of the bearing in the axial direction. Other exemplary bearings, arrangements and methods are also disclosed.
1. A turbocharger comprising a semi-floating bearing, the bearing comprising:
a central axis defining a cylindrical coordinate system with an axial direction, a radial direction and an angular direction;
a turbine end;
a compressor end;
journal surfaces between the turbine end and the compressor end, the journal surfaces configured to support a turbocharger shaft; and
an opening disposed between the turbine end and the compressor end, the opening having a radial dimension that exceeds an axial dimension to, upon receipt of a locating pin, provide for movement of the bearing in the angular direction about its central axis and to provide for lesser movement of the bearing in the axial direction.
2. The turbocharger of claim 1 further comprising a locating pin.
3. The turbocharger of claim 2 wherein the locating pin comprises a locating region with a diameter approximately equal to the axial dimension of the opening.
4. An assembly comprising:
a center housing that comprises a through bore extending from a turbine end to a compressor end;
a locating pin; and
a semi-floating bearing disposed in the bore, wherein the semi-floating bearing comprises
a central axis defining a cylindrical coordinate system with an axial direction, a radial direction and an angular direction,
journal surfaces between a turbine end and a compressor end of the semi-floating bearing, the journal surfaces configured to support a turbocharger shaft, and
an opening disposed between the turbine end and the compressor end of the semi-floating bearing, the opening having a radial dimension that exceeds an axial dimension to, upon receipt of the locating pin, provide for movement of the semi-floating bearing in the angular direction about its central axis and to provide for lesser movement of the semi-floating bearing in the axial direction.
5. A method comprising:
providing a semi-floating bearing located in a bore of a center housing with a locating pin wherein the semi-floating bearing comprises
a central axis defining a cylindrical coordinate system with an axial direction, a radial direction and an angular direction,
journal surfaces between a turbine end and a compressor end of the semi-floating bearing, the journal surfaces configured to support a turbocharger shaft, and
an opening disposed between the turbine end and the compressor end of the semi-floating bearing, the opening having a radial dimension that exceeds an axial dimension;
rotating the turbocharger shaft supported by the semi-floating bearing; and
without axially translating the semi-floating bearing in the bore of the center housing, rotating the semi-floating bearing in the bore of the center housing.
6. The method of claim 5 wherein rotating the semi-floating bearing reduces noise generation.
7. The method of claim 5 further comprising providing a lubricant film between the semi-floating bearing and the center housing.
8. The method of claim 7 wherein rotating the semi-floating bearing stabilizes the lubricant film.
9. The method of claim 5 further comprising balancing the turbocharger shaft, a compressor wheel and a turbine wheel supported by the semi-floating bearing disposed in the bore of the center housing.