Turbocharger shaft bearing
AssigneeThe Garrett Corporation
InventorJames E. T. Blake
Life of this patent
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Abstract
A bearing for supporting a turbocharger shaft comprises a one-piece cylindrical bearing sleeve for rotational floating between a turbocharger housing and shaft. The bearing includes an inner diameter configured to define a plurality of axially extending arcuate lands formed on a common radius and separated by oil-receiving recesses.
Claims11
A rotationally floating shaft bearing for use in a turbocharger, comprising a generally cylindrical unitary sleeve having a generally circular outer diameter, and an inner diameter defining at least three equiangularly arranged and substantially identical arcuate lands formed on a common radius and separated by a corresponding plurality of substantially identical arcuate recesses formed on a common radius slightly greater than the radius of said lands, said lands and recesses being formed on a common center and extending axially the length of said sleeve, said recesses having a total arcuate width of from about one to about three times the total arcuate width of said lands, and said sleeve having formed therein a plurality of radially extending holes in alignment centrally with respect to the arcuate widths of respective ones of said recesses for communicating lubricating oil centrally into said recesses.
In a turbocharger having a turbocharger center housing with a bearing bore formed therein, and a rotatable shaft received axially through said bearing bore, a turbocharger shaft bearing, comprising a generally cylindrical floating unitary sleeve received into said bearing bore for rotation with respect to said bearing bore and for receiving said shaft therethrough, said sleeve having a generally circular outer diameter and an inner diameter defining an equiangularly arranged plurality of at least three substantially identical arcuate lands formed on a common radius for rotatably supporting said shaft, said lands being separated by a corresponding number of substantially identical arcuate recesses formed on a common radius slightly greater than the radius of said lands, said lands and recesses extending the axial length of said sleeve and sharing a common centerline with said bearing bore, said recesses having a total arcuate width of about three times the total arcuate width of said lands, and said sleeve having formed therein a plurality of radially extending holes in alignment centrally with respect to the arcuate widths of respective ones of said recesses for communicating lubricating oil into said recesses.
In a turbocharger having a turbocharger center housing with a bearing bore formed therein, and a rotatable shaft received axially through the bearing bore, a method of supporting the shaft against radial excursions at relatively high speed shaft rotation, comprising the steps of mounting a unitary bearing sleeve within the bore for reception of the shaft and for rotational floating with respect to the housing and the shaft;
- configuring the sleeve outer diameter to define a generally circular profile;
- configuring the sleeve inner diameter to define an eqiangularly arranged plurality of at least three substantially identical arcuate lands extending the axial length of the sleeve and formed on a common center for rotatably supporting the shaft, and a corresponding plurality of substantially identical arcuate recesses extending the axial length of the sleeve and separating the lands and formed on a common radius slightly greater than the radius of the lands, wherein the arcuate width of the recesses is from about one to about three times the arcuate width of the lands;
- forming in the sleeve a plurality of radially extending holes in alignment centrally with the arcuate widths of respective ones of the recesses;
- and supplying lubricating oil through passage means in the housing to the sleeve for passage through the holes centrally into the recesses.
In a turbocharger having a turbocharger center housing with a bearing bore formed therein, and a rotatable shaft axially received through the bearing bore, a method of supporting the shaft against radial excursions at relatively high speed shaft rotation, comprising the steps of mounting a bearing sleeve within the bore for reception of the shaft with an outer diameter clearance approximately twice the inner diameter clearance for rotational floating of the sleeve with respect to the housing and the shaft;
- configuring the sleeve outer diameter to have a generally circular profile;
- configuring the sleeve inner diameter to define a plurality of at least three arcuate lands extending the axial length of the sleeve and formed on a common center for rotatably supporting the shaft, and a corresponding plurality of arcuate recesses extending the axial length of the sleeve and separating the lands and formed on a common radius slightly greater than the radius of the lands, wherein the arcuate width of the recesses is from about one time to about three times the arcuate width of the lands;
- forming in the sleeve a plurality of radially extending holes in alignment centrally with the arcuate width and axial lengths of respective ones of the recesses;
- forming a circumferential groove about the sleeve in substantial axial alignment with the radial holes;
- supplying lubricating oil through passage means in the housing to the sleeve via the groove for passage through the holes centrally into the recesses;
- and slinging particulate in the lubricating oil radially outwardly into the groove away from the sleeve upon rotational floating of the sleeve.
Dependencies are inferred from the claim text.