Axial bearing arrangement

Patent metadata

Field	Value
Publication number	US-9638244-B2
Application number	US-201314398137-A
Country	US
Kind code	B2
Filing date	Apr 29, 2013
Priority date	May 8, 2012
Publication date	May 2, 2017
Grant date	May 2, 2017

Abstract

A hydrodynamic axial bearing is provided with segments arranged on a circular ring on axial bearings, wherein a plurality of pressure fields are built up. The length of the individual segments is defined in the circumferential direction, between a first edge and a second edge. The first edge delimits the wedge surface of the segments. In fast-rotating bearings, the ratio of segment width to segment length has a decisive influence on the attainable load-bearing capacity and resulting friction losses. The load-bearing capacity and friction losses are improved by increasing the segment length more intensely with increasing radius. The first edge does not run straight but rather has steps, is arcuate or has linear portions with different gradients.

First claim

The invention claimed is:

1. An axial bearing arrangement ( 11 ) for a rotating shaft ( 10 ) which extends in an axial direction, comprising
a non-rotating axial bearing ( 3 ) having a bearing surface ( 24 ), having a plurality of surface segments ( 25 ) which are distributed along the circumferential direction and which project from or are recessed into the bearing surface ( 24 ) of the axial bearing ( 3 ) in the axial direction, and
a run-on collar ( 12 , 13 ) which is rotationally conjointly connected to the shaft ( 10 ), wherein the run-on collar ( 12 , 13 ) comprises an annular load-bearing surface ( 15 ) for support on the segments ( 25 ) of the axial bearing,
wherein the segments ( 25 ) are delimited, with respect to the direction of rotation of the rotating shaft ( 10 ) and run-on collar ( 12 , 13 ), by in each case one first edge ( 36 ) and one second edge ( 37 ), wherein a segment length ( 35 ) is defined as an arc length between the first and second edges ( 36 , 37 ) in the circumferential direction, wherein a radius (r) is defined perpendicular to the axial direction to the central point ( 34 ) of the shaft ( 10 ), and wherein each segment has a segment width ( 31 ) delimited by a radially inner edge and a radially outer edge, and
wherein the segment length ( 35 ) relative to the radius increases with increasing radius (r) at a rate greater than the increase in radius over at least a portion of the segment width ( 31 ), and
wherein the first edge ( 36 ) has at least two linear parts with different gradient.

2. An axial bearing arrangement ( 11 ) for a rotating shaft ( 10 ) which extends in an axial direction, comprising
a non-rotating axial bearing ( 3 ) having a bearing surface ( 24 ), having a plurality of surface segments ( 25 ) which are distributed along the circumferential direction and which project from or are recessed into the bearing surface ( 24 ) of the axial bearing ( 3 ) in the axial direction, and
a run-on collar ( 12 , 13 ) which is rotationally conjointly connected to the shaft ( 10 ), wherein the run-on collar ( 12 , 13 ) comprises an annular load-bearing surface ( 15 ) for support on the segments ( 25 ) of the axial bearing,
wherein the segments ( 25 ) are delimited, with respect to the direction of rotation of the rotating shaft ( 10 ) and run-on collar ( 12 , 13 ), by in each case one first edge ( 36 ) and one second edge ( 37 ), wherein a segment length ( 35 ) is defined as an arc length between the first and second edges ( 36 , 37 ) in the circumferential direction, wherein a radius (r) is defined perpendicular to the axial direction to the central point ( 34 ) of the shaft ( 10 ), and wherein each segment has a segment width ( 31 ) delimited by a radially inner edge and a radially outer edge, and
wherein the segment length ( 35 ) relative to the radius increases with increasing radius (r) at a rate greater than the increase in radius over at least a portion of the segment width ( 31 ),
wherein each segment ( 25 ) is formed from a rest surface ( 27 ) and a hydrodynamically acting wedge surface or stepped surface ( 26 ) positioned downstream, with respect to the direction of rotation of the rotating shaft ( 10 ) and run-on collar ( 12 , 13 ), of said rest surface, wherein said wedge surface or stepped surface forms a narrowing lubrication gap which ensures the hydrodynamic load-bearing capacity of the axial bearing arrangement during operation, and
wherein the segment length ( 35 ) is made up of a wedge length ( 32 ) of the wedge surface ( 26 ) and a rest length ( 33 ) of the rest surface ( 27 ), wherein the wedge length ( 32 ) increases with increasing radius (r).

3. The axial bearing arrangement as claimed in claim 2 , wherein the rest surface ( 27 ) is arranged parallel to the load-bearing surface ( 15 ).

4. The axial bearing arrangement as claimed in claim 2 , wherein the segment length ( 35 ) is made up of a wedge length ( 32 ) of the wedge surface ( 26 ) and a rest length ( 33 ) of the rest surface ( 27 ), wherein the wedge length ( 32 ) and also the rest length ( 33 ) increase with increasing radius (r).

5. An axial bearing arrangement ( 11 ) for a rotating shaft ( 10 ) which extends in an axial direction, comprising
a non-rotating axial bearing ( 3 ) having a bearing surface ( 24 ), having a plurality of surface segments ( 25 ) which are distributed along the circumferential direction and which project from or are recessed into the bearing surface ( 24 ) of the axial bearing ( 3 ) in the axial direction, and
a run-on collar ( 12 , 13 ) which is rotationally conjointly connected to the shaft ( 10 ), wherein the run-on collar ( 12 , 13 ) comprises an annular load-bearing surface ( 15 ) for support on the segments ( 25 ) of the axial bearing,
wherein the segments ( 25 ) are delimited, with respect to the direction of rotation of the rotating shaft ( 10 ) and run-on collar ( 12 , 13 ), by in each case one first edge ( 36 ) and one second edge ( 37 ), wherein a segment length ( 35 ) is defined as an arc length between the first and second edges ( 36 , 37 ) in the circumferential direction, wherein a radius (r) is defined perpendicular to the axial direction to the central point ( 34 ) of the shaft ( 10 ), and wherein each segment has a segment width ( 31 ) delimited by a radially inner edge and a radially outer edge, and
wherein the segment length ( 35 ) relative to the radius increases with increasing radius (r) at a rate greater than the increase in radius over at least a portion of the segment width ( 31 ), and
wherein the first edge ( 36 ) has at least one first arcuate part and at least one second arcuate part, different from the first arcuate part.

6. A turbocharger ( 1 ), comprising at least one axial bearing arrangement ( 11 ) for a rotating shaft ( 10 ) which extends in an axial direction, the axial bearing arrangement ( 11 ) comprising
a non-rotating axial bearing ( 3 ) having a bearing surface ( 24 ), having a plurality of surface segments ( 25 ) which are distributed along the circumferential direction and which project from or are recessed into the bearing surface ( 24 ) of the axial bearing ( 3 ) in the axial direction, and
a run-on collar ( 12 , 13 ) which is rotationally conjointly connected to the shaft ( 10 ), wherein the run-on collar ( 12 , 13 ) comprises an annular load-bearing surface ( 15 ) for support on the segments ( 25 ) of the axial bearing,
wherein the segments ( 25 ) are delimited, with respect to the direction of rotation of the rotating shaft ( 10 ) and run-on collar ( 12 , 13 ), by in each case one first edge ( 36 ) and one second edge ( 37 ), wherein a segment length ( 35 ) is defined as an arc length between the first and second edges ( 36 , 37 ) in the circumferential direction, wherein a radius (r) is defined perpendicular to the axial direction to the central point ( 34 ) of the shaft ( 10 ), and wherein each segment has a segment width ( 31 ) delimited by a radially inner edge and a radially outer edge,
wherein the segment length ( 35 ) relative to the radius increases with increasing radius (r) at a rate greater than the increase in radius over at least a portion of the segment width ( 31 ), and
wherein the first edge ( 36 ) has at least two steps.

7. The turbocharger as claimed in claim 6 , wherein the turbocharger is an exhaust-gas turbocharger.

Assignees

• Borgwarner Inc

Inventors

• Duecker-Schulz Thomas
• Koerner Thomas

Classifications

• F16C17/047

  with fixed wedges to generate hydrodynamic pressure · CPC title

• F05D2240/52

  Axial thrust bearings · CPC title

• F16C33/107

  Grooves for generating pressure · CPC title

• F16C2360/24

  Turbochargers · CPC title

• F05D2220/40

  in turbochargers · CPC title