Tapered land thrust bearing device and turbocharger provided with the bearing device

Patent metadata

Field	Value
Publication number	US-10072707-B2
Application number	US-201415113894-A
Country	US
Kind code	B2
Filing date	Feb 27, 2014
Priority date	Feb 27, 2014
Publication date	Sep 11, 2018
Grant date	Sep 11, 2018

Abstract

A tapered land thrust bearing device with a land surface having a substantially reduced area without changing the contour shape of the land surface even if the area of the land surface is small, and high mechanical efficiency, as well as a turbocharger provided with the bearing device. A tapered land thrust bearing device includes: a flange portion fitted onto a rotary shaft and including a first thrust portion; and a thrust member including a second thrust portion which is disposed around a through hole and which faces the first thrust portion of the flange portion.

First claim

The invention claimed is:

1. A tapered land thrust bearing device, comprising:
a rotary shaft;
a flange portion fitted onto the rotary shaft and including a first thrust portion; and
a thrust member including a through hole through which the rotary shaft is inserted and a second thrust portion which is disposed around the through hole and which faces the first thrust portion of the flange portion,
wherein one of the first thrust portion or the second thrust portion includes
a plurality of land surfaces each of which is parallel to a plane orthogonal to an axis of the rotary shaft, the land surfaces being disposed at intervals in a circumferential direction of the through hole,
a plurality of tapered surfaces each of which is disposed between the plurality of land surfaces, joined via a step to a first boundary of one of the land surfaces on one side in the circumferential direction of the through hole, and joined continuously to a second boundary of another one of the land surfaces on the other side in the circumferential direction of the through hole, and
at least one concave portion disposed on each of the plurality of land surfaces,

wherein the at least one concave portion comprises a plurality of concave portions,
wherein the plurality of concave portions comprises a plurality of first concave portions disposed along a radial direction of the through hole,
wherein, on each of the plurality of land surfaces, the plurality of first concave portions are disposed within a region of from 10% to 20% of an angle formed by the adjacent first and second boundaries in the circumferential direction from the second boundary of the land surface, and
wherein each of the plurality of first concave portions has a depth within a range of from 0.001 mm to 0.025 mm.

2. The tapered land thrust bearing device according to claim 1 ,
wherein the plurality of land surfaces comprises three or more land surfaces,
wherein a diameter of an outer circumference of the plurality of land surfaces is not more than 15 mm, and
wherein an inclination angle of the tapered surfaces is within a range of from 1 e-5° to 1.0°.

3. The tapered land thrust bearing device according to claim 1 , wherein opening areas of the first concave portions increase outward in stages in the radial direction of the through hole.

4. A turbocharger, comprising: a tapered land thrust bearing device according to claim 1 ; a centrifugal compressor including an impeller; and a turbine including a turbine blade, wherein the turbine blade and the impeller are coupled to each other via the rotary shaft.

5. A tapered land thrust bearing device, comprising:
a rotary shaft;
a flange portion fitted onto the rotary shaft and including a first thrust portion; and
a thrust member including a through hole through which the rotary shaft is inserted and a second thrust portion which is disposed around the through hole and which faces the first thrust portion of the flange portion,
wherein one of the first thrust portion or the second thrust portion includes
a plurality of land surfaces each of which is parallel to a plane orthogonal to an axis of the rotary shaft,
the land surfaces being disposed at intervals in a circumferential direction of the through hole,
a plurality of tapered surfaces each of which is disposed between the plurality of land surfaces, joined via a step to a first boundary of one of the land surfaces on one side in the circumferential direction of the through hole, and joined continuously to a second boundary of another one of the land surfaces on the other side in the circumferential direction of the through hole, and
at least one concave portion disposed on each of the plurality of land surfaces,
wherein the at least one concave portion comprises a plurality of concave portions,
wherein the plurality of concave portions are disposed along the radial direction and the circumferential direction of the through hole,
wherein a plurality of first concave portions disposed along the radial direction of the through hole are a part of the plurality of concave portions,
wherein, on each of the plurality of land surfaces, the plurality of first concave portions are disposed within a region of from 10% to 20% of an angle formed by the adjacent first and second boundaries in the circumferential direction from the first or second boundary of the land surface, and
wherein each of the plurality of first concave portions has a depth within a range of from 0.001 mm to 0.025 mm.

6. The tapered land thrust bearing device according to claim 5 , wherein depths of the plurality of concave portions change in stages along the circumferential direction of the through hole.

7. The tapered land thrust bearing device according to claim 5 ,
wherein the plurality of land surfaces comprises three or more land surfaces,
wherein a diameter of an outer circumference of the plurality of land surfaces is not more than 15 mm, and wherein an inclination angle of the tapered surfaces is with a range of from 1e-5° to 1.0°.

8. A turbocharger, comprising:
a tapered land thrust bearing device according to claim 5 ;
a centrifugal compressor including an impeller; and
a turbine including a turbine blade,
wherein the turbine blade and the impeller are coupled to each other via the rotary shaft.

9. A tapered land thrust bearing device, comprising a rotary shaft;
a flange portion fitted onto the rotary shaft and including a first thrust portion, and
a thrust member including a through hole through which the rotary shaft is inserted and a second thrust portion which is disposed around the through hole and which faces the first thrust portion of the flange portion,
wherein one of the first thrust portion or the second thrust portion includes
a plurality of land surfaces each of which is parallel to a plane orthogonal to an axis of the rotary shaft,
the land surfaces being disposed at intervals in a circumferential direction of the through hole,
a plurality of tapered surfaces each of which is disposed between the plurality of land surfaces, joined via a step to a first boundary of one of the land surfaces on one side in the circumferential direction of the through hole, and joined continuously to a second boundary of another one of the land surfaces on the other side in the circumferential direction of the through hole, and
at least one concave portion disposed on each of the plurality of land surfaces,
wherein the at least one concave portion comprises a plurality of concave portions; and
wherein the plurality of concave portions are disposed in a spiral pattern or a herringbone pattern.

10. The tapered land thrust bearing device according to claim 9 ,
wherein the plurality of land surfaces comprises three or more land surfaces,
wherein a diameter of an outer circumference of the plurality of land surfaces is not more than 15 mm, and wherein an inclination angle of the tapered surfaces is within a range of from 1e-5° to 1.0°.

11. A turbocharger, comprising:
a tapered land thrust bearing device according to claim 9 ;
a centrifugal compressor including an impeller; and
a turbine including a turbine blade,
wherein the turbine blade and the impeller are coupled to each other via the rotary shaft.

12. A tapered land thrust bearing device, comprising:
a rotary shaft;
a flange portion fitted onto the rotary shaft and including a first thrust portion; and
a thrust member including a through hole through which the rotary shaft is inserted and a second thrust portion which is disposed around the through hole and which faces the first thrust portion of the flange portion,
wherein one of the first thrust port

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Futae Takaya
• Nishida Hideaki

Classifications

• F16C17/18

  with floating brasses or brushing, rotatable at a reduced speed {(F16C17/03, F16C17/06 take precedence)} · CPC title

• F05D2250/182

  crenellated, notched · CPC title

• F16C33/128

  Porous bearings, e.g. bushes of sintered alloy · CPC title

• F16C2360/24

  Turbochargers · CPC title

• F05D2250/191

  perforated · CPC title