Oil-drain device for thrust bearing device and turbocharger provided with the same

• US 10,473,207 B2
• Filed: 12/18/2014
• Issued: 11/12/2019
• Est. Priority Date: 12/18/2014
• Status: Active Grant

• Current Assignee: Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. (Mitsubishi Heavy Industries, Ltd.)
• Original Assignee: Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. (Mitsubishi Heavy Industries, Ltd.)
• Inventors: Nishioka, Tadasuke, Danmoto, Yosuke, Tomita, Isao, Nambu, Takashi, Akiyama, Yoji, Kojima, Yuya, Ishizaki, Tatsuya, Yano, Seigi, Futae, Takaya, Ebisu, Motoki
• Primary Examiner(s): Dondero, William E
• Assistant Examiner(s): Reese, Robert T
• Application Number:
  US15/515,332
• Publication Number:
  US 20170276233A1
• Time in Patent Office: 1,790 Days
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F02B 39/14 Lubrication of pumps; Safety measures therefor
• CPC Class Codes: F04D 29/056 Bearings
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F16C 17/04 for axial load only
• CPC Class Codes: F16C 2360/24 Turbochargers in general F02C6/12
• CPC Class Codes: F16C 33/1025 with liquid, e.g. oil, as lubricant
• CPC Class Codes: F16H 57/0409 characterised by the problem to increase efficiency, e.g. by reducing splash losses
• CPC Class Codes: F16H 57/042 Guidance of lubricant

Abstract

An oil-drain device for a thrust bearing includes: a rotor shaft; a collar member mounted to an outer periphery of the rotor shaft; a thrust bearing supporting the rotor shaft in an axial direction; and an oil-drain space forming member defining an oil-drain space through which lubricant oil leaking from a sliding portion of the thrust bearing flows, between the thrust bearing and the oil-drain space forming member. The oil-drain space includes: an oil-drain channel defined between a first end surface of the thrust bearing and a first end surface of the oil-drain space forming member, surrounding the flange portion of the collar member; and an oil-drain port formed below the oil-drain channel, for discharging the lubricant oil flowing through the oil-drain channel outside the oil-drain space. The oil-drain space is configured to guide the lubricant oil flowing through the oil-drain channel to outside the oil-drain space via the oil-drain port, along a flow direction of the lubricant oil flowing through the oil-drain channel from an upstream side toward a downstream side in a rotational direction of the rotor shaft.

Claims

1. An oil-drain device for a thrust bearing, comprising:

a rotor shaft;

a collar member to be mounted to an outer periphery of the rotor shaft so as to be rotatable with the rotor shaft, the collar member having a collar body portion having a cylindrical shape and a flange portion formed to have a larger diameter than the collar body portion;

a thrust bearing having an insertion hole into which the rotor shaft is inserted, the thrust bearing being configured to make slide contact with a first end surface of the flange portion of the collar member to support the rotor shaft which rotates in a state of being inserted into the insertion hole in an axial direction;

an oil-supply channel for supplying lubricant oil to a sliding portion of the thrust bearing which makes slide contact with the first end surface of the flange portion; and

an oil-drain space forming member disposed on a side of a first end surface of the thrust bearing, the oil-drain space forming member defining an oil-drain space through which the lubricant oil leaking from the sliding portion of the thrust bearing flows, between the thrust bearing and the oil-drain space forming member,

wherein the oil-drain space includes;

an oil-drain channel defined between the first end surface of the thrust bearing and a first end surface of the oil-drain space forming member, the oil-drain channel surrounding the flange portion of the collar member; and

an oil-drain port formed below the oil-drain channel, for discharging the lubricant oil flowing through the oil-drain channel outside the oil-drain space,

wherein the oil-drain space forming member at least comprises a body portion including;

a center hole into which the collar body portion of the collar member mounted to the rotor shaft is inserted;

an inner peripheral edge portion which makes slide contact with a second end surface of the flange portion of the collar member at a radially outer side of the center hole;

an intermediate portion formed on a radially outer side of the inner peripheral edge portion, with a gap from the first end surface of the thrust bearing; and

an outer peripheral edge portion configured to make contact with the first end surface of the thrust bearing at a radially outer side of the intermediate portion,

wherein the oil-dram port is formed by a portion at a lower end body portion, the portion not having the outer peripheral edge portion formed thereon, and

wherein the outer peripheral edge portion includes;

an arc shaped portion extending in an arc shape from an upstream edge of the outer peripheral edge portion toward a predetermined position upstream of the oil drain-port in the rotational direction, and

a linear portion extending from the predetermined position in the arc-shaped portion to the oil-drain port along a tangent direction at the predetermined position.

2. The oil-drain device for a thrust bearing according to claim 1, further comprising a retainer disposed on a side of a second end surface of the oil-drain space forming member, and configured to retain the oil-drain space forming member and the thrust bearing on a radially outer side of the rotor shaft, and

wherein the retainer includes an inclined surface below the oil-drain port, the inclined surface extending obliquely downward toward the thrust bearing.

3. The oil-drain device for a thrust bearing according to claim 1,

wherein the intermediate portion of the oil-drain space forming member includes a recessed portion configured such that a gap from the first end surface of the thrust bearing is greater at the recessed portion than at other part of the intermediate portion, and

wherein the oil-drain channel includes an oil-drain groove extending in a circumferential direction formed by the recessed portion.

4. The oil-drain device for a thrust bearing according to claim 3,

wherein the oil-drain space forming member further includes a plurality of guide plates disposed at intervals in a circumferential direction inside the oil-drain channel, for guiding the lubricant oil flowing through the oil-drain channel to the oil-drain groove.

5. The oil-drain device for a thrust bearing according to claim 4,

wherein the guide plates extend radially inward from a peripheral edge portion of the oil-drain space forming member,

wherein leading edges of the guide plates are disposed closer to the thrust bearing than trailing edges of the guide plates, and

wherein an intersection between each of the leading edges and the peripheral edge portion is positioned upstream, in the flow direction, of an intersection between a corresponding one of the trailing edges and the peripheral edge portion.

6. The oil-drain device for a thrust bearing according to claim 1,

wherein the oil-drain space forming member has a second oil-drain port communicating with the oil-drain channel and is configured such that the lubricant oil flowing through the oil-drain channel is discharged outside the oil-drain space via the second oil-drain port.

7. The oil-drain device for a thrust bearing according to claim 6,

wherein the second oil-drain port has an opening which faces the flow direction of the lubricant oil flowing through the oil-drain channel, at an upper part of the oil-drain space forming member.

8. The oil-drain device for a thrust bearing according to claim 1,

wherein a groove portion extending in a circumferential direction is formed on the first end surface of the thrust bearing at a position radially outside an outer peripheral end surface of the flange portion, and

wherein the first end surface of the thrust bearing comprises an outer first end surface disposed on a radially outer side of the groove portion and an inner first end surface disposed on a radially inner side of the groove portion, the outer first end surface protruding toward the oil-drain space forming member to be closer to the oil-drain space forming member than the inner first end surface.

9. The oil-drain device or a thrust bearing according to claim 1,

wherein the oil-drain port is formed in an upstream region, in the rotational direction, of a centerline extending in an upward and downward direction through a rotational center of the rotor shaft.

10. The oil-drain device for a thrust bearing according to claim 1,

wherein the oil-drain space forming member comprises:

a body portion including;

a center hole into which the collar body portion of the collar member mounted to the rotor shaft is inserted;

an inner peripheral edge portion which makes slide contact with a second end surface of the flange portion of the collar member at a radially outer side of the center hole;

an intermediate portion formed on a radially outer side of the inner peripheral edge portion, with a gap from the first end surface of the thrust bearing; and

an outer peripheral edge portion configured to make contact with the first end surface of the thrust bearing at a radially outer side of the intermediate portion; and

a tongue portion extending obliquely downward from a lower end of the body portion toward the thrust bearing,

wherein the oil-drain port is formed by a portion of the lower end of the body portion, the portion not having the outer peripheral edge portion formed thereon,

wherein the tongue portion includes a bend portion bended to close the oil-drain port in a downstream region, in the rotational direction, of the center line.

11. The oil-drain device for a thrust bearing according to claim 1,

wherein the oil-drain channel is formed to have a flow-path cross sectional area which increases in the rotational direction from an upstream edge toward a downstream edge of the outer peripheral edge portion.

12. The oil-drain device for a thrust bearing according to claim 1,

wherein the oil-drain space forming member comprises an oil deflector formed from sheet metal.

13. A turbocharger, comprising:

a turbine impeller disposed on an end side of the rotor shaft;

a compressor impeller disposed on another end side of the rotor shaft; and

the oil-drain device for a thrust bearing according to claim 1.

14. An oil-drain device for a thrust bearing comprising,

a rotor shaft;

a collar member to be mounted to an outer periphery of the rotor shaft so as to be rotatable with the rotor shaft, the collar member having a collar body portion having a cylindrical shape and a flange portion formed to have a larger diameter than the collar body portion;

a thrust bearing having an insertion hole into which the rotor shaft is inserted, the thrust bearing being configured to make slide contact with a first end surface of the flange portion of the collar member to support the rotor shaft which rotates in a state of being inserted into the insertion hole in an axial direction;

an oil-supply channel for supplying lubricant oil to a sliding portion of the thrust bearing which makes slide contact with the first end surface of the flange portion; and

an oil-drain space forming member disposed on a side of a first end surface of the thrust bearing, the oil-drain space forming member defining an oil-drain space through which the lubricant oil leaking from the sliding portion of the thrust bearing flows, between the thrust bearing and the oil-drain space forming member,

wherein the oil-drain space includes;

an oil-drain channel defined between the first end surface of the thrust bearing and a first end surface of the oil-drain space forming member, the oil-drain channel surrounding the flange portion of the collar member; and

an oil-drain port formed below the oil-drain channel, for discharging the lubricant oil flowing through the oil-drain channel outside the oil-drain space,

wherein the oil-drain space forming member comprises;

a body portion including;

a center hole into which the collar body portion of the collar member mounted to the rotor shaft is inserted;

an inner peripheral edge portion which makes slide contact with a second end surface of the flange portion of the collar member at a radially outer side of the center hole;

an intermediate portion formed on a radially outer side of the inner peripheral edge portion, with a gap from the first end surface of the thrust bearing; and

an outer peripheral edge portion configured to make contact with the first end surface of the thrust bearing at a radially outer side of the intermediate portion; and

a tongue portion extending obliquely downward from a lower end of the body portion toward the thrust bearing,

wherein the oil-drain port is formed by a portion of the lower end of the body portion, the portion not having the outer peripheral edge portion formed thereon, and

wherein the tongue portion is formed so as to increase a height of the oil-drain port from a side of a downstream edge toward a side of an upstream edge gradually, the height of the oil-drain port being defined as a vertical distance between the thrist bearing and the tongue portion.

15. A turbocharger, comprising:

a turbine impeller disposed on an end side of the rotor shaft;

a compressor impeller disposed on another end side of the rotor shaft; and

the oil-drain device for a thrust bearing according to claim 14.