CN203835977U - Thrust bearing - Google Patents

Thrust bearing Download PDF

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Publication number
CN203835977U
CN203835977U CN201420260090.3U CN201420260090U CN203835977U CN 203835977 U CN203835977 U CN 203835977U CN 201420260090 U CN201420260090 U CN 201420260090U CN 203835977 U CN203835977 U CN 203835977U
Authority
CN
China
Prior art keywords
bearing
retainer
circular
roller path
raceway circle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201420260090.3U
Other languages
Chinese (zh)
Inventor
寺田和晃
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NSK Ltd
Original Assignee
NSK Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by NSK Ltd filed Critical NSK Ltd
Priority to CN201420260090.3U priority Critical patent/CN203835977U/en
Application granted granted Critical
Publication of CN203835977U publication Critical patent/CN203835977U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Rolling Contact Bearings (AREA)

Abstract

The utility model relates to a thrust bearing. The thrust bearing is specifically composed of a pair of circular-ring-shaped roller path rings, multiple relatively moving cylindrical rolling bodies arranged in the circular-ring-shaped roller path rings and a circular-ring-shaped retainer separating the rolling bodies at intervals. The end portion of the inner peripheral side of the retainer is provided with a guiding portion facing the roller path rings on one side and protruding in the direction of a rotating shaft, and the proportion X of the protruding amount of the guiding portion extending from the bearing inner diameter relative to the inner diameters of the roller path rings is 0.2%<=X<=3.0%, and the proportion Y of the protruding amount of the guiding portion extending from the bearing outer side end faces of the rolling bodies relative to the outer diameters of the roller path rings is 0.5%<=Y<=2.5%. Therefore, the sliding resistance of the thrust bearing in high-speed rotation is reduced, the rotation stability is improved, and the lubricating performance is improved.

Description

Thrust-bearing
Technical field
The utility model relates to the thrust-bearing for High Rotation Speed etc.
Background technique
From in the past, the performances such as slip resistance reduction, rotational stabilization raising and lubricity raising under the High Rotation Speed of thrust-bearing improve and just become problem.
Model utility content
In order to solve above-mentioned problem, the utility model provides a kind of thrust-bearing, and it has: running shaft is configured in coaxial a pair of circular raceway circle, the multiple cylindric rolling element of also mutual relative movement between a pair of described raceway circle, with the circular retainer that multiple described rolling elements are equally spaced kept, described thrust-bearing is characterised in that, on the end, inner circumferential side of described retainer, there is described raceway circle towards a side along the outstanding guide portion of described running shaft direction, and, be formed as, described guide portion is 0.2%≤X≤3.0% from the overhang of bearing bore diameter with respect to the ratio X of described raceway circle internal diameter, retainer is 0.5%≤Y≤2.5% from the overhang of end face outside the bearing of described rolling element with respect to the ratio Y of described raceway circle external diameter, thus, the slip resistance that can realize under the High Rotation Speed of thrust-bearing reduces, rotational stabilization improves and lubricity improves.
Brief description of the drawings
Fig. 1 is the sectional view that represents thrust-bearing of the present utility model.
Embodiment
The thrust-bearing 1 of present embodiment has: running shaft is configured in coaxial a pair of circular raceway circle 2; The multiple cylindric rolling element 3 of also mutual relative movement between above-mentioned a pair of raceway circle; With the circular retainer 4 that above-mentioned multiple rolling elements are equally spaced kept.Above-mentioned raceway circle 2 is toroidal, on the axial surface of rotation, is formed with rolling surface.Above-mentioned retainer 4 has multiple pockets hole of accommodating rolling element 3, has the guide portion 4a that gives prominence to and engage with raceway circle inner peripheral surface along above-mentioned running shaft direction towards the raceway circle of one side on end, inner circumferential side.And, be formed as, guide sections is 0.2%≤X≤3.0% from the overhang a of bearing bore diameter with respect to the ratio X of above-mentioned raceway circle inner diameter D 1, retainer is 0.5%≤Y≤2.5% from the overhang b of end face outside the bearing of above-mentioned rolling element with respect to the ratio Y of above-mentioned raceway circle outer diameter D 2, thus, in the time that thrust-bearing carries out High Rotation Speed, make the lubricity optimization of slip resistance, rotational stabilization and thrust-bearing, the performance that can realize bearing improves.In addition, in the utility model, bearing bore diameter being made as to 540mm~3200mm and bearing outside diameter being made as in the using scope of 662mm~3400mm, obviously show performance and improve.And, arrange the oiling agent feed path running through in retainer towards rolling surface side and guide surface exterior side by the internal side diameter from retainer, and expect further to improve the lubricity on slip surface.

Claims (1)

1. a thrust-bearing, it has: running shaft is configured in coaxial a pair of circular raceway circle, the multiple cylindric rolling element of also mutual relative movement between a pair of described raceway circle, with the circular retainer that multiple described rolling elements are equally spaced kept, described thrust-bearing is characterised in that, on the end, inner circumferential side of described retainer, there is described raceway circle towards a side along the outstanding guide portion of described running shaft direction, and, be formed as, described guide portion is 0.2%≤X≤3.0% from the overhang (a) of bearing bore diameter with respect to the ratio X of described raceway circle internal diameter (D1), retainer is 0.5%≤Y≤2.5% from the overhang (b) of end face outside the bearing of described rolling element with respect to the ratio Y of described raceway circle external diameter (D2).
CN201420260090.3U 2014-05-21 2014-05-21 Thrust bearing Expired - Fee Related CN203835977U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420260090.3U CN203835977U (en) 2014-05-21 2014-05-21 Thrust bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420260090.3U CN203835977U (en) 2014-05-21 2014-05-21 Thrust bearing

Publications (1)

Publication Number Publication Date
CN203835977U true CN203835977U (en) 2014-09-17

Family

ID=51513824

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420260090.3U Expired - Fee Related CN203835977U (en) 2014-05-21 2014-05-21 Thrust bearing

Country Status (1)

Country Link
CN (1) CN203835977U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111720449A (en) * 2020-05-28 2020-09-29 南通德元机械制造有限公司 Precise thrust bearing and assembling method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111720449A (en) * 2020-05-28 2020-09-29 南通德元机械制造有限公司 Precise thrust bearing and assembling method thereof
CN111720449B (en) * 2020-05-28 2021-12-21 南通德元机械制造有限公司 Precise thrust bearing and assembling method thereof

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140917

Termination date: 20210521