CN2900796Y - Thrust bearing of turbocharger - Google Patents

Thrust bearing of turbocharger Download PDF

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Publication number
CN2900796Y
CN2900796Y CN 200620012192 CN200620012192U CN2900796Y CN 2900796 Y CN2900796 Y CN 2900796Y CN 200620012192 CN200620012192 CN 200620012192 CN 200620012192 U CN200620012192 U CN 200620012192U CN 2900796 Y CN2900796 Y CN 2900796Y
Authority
CN
China
Prior art keywords
bearing
plane
thrust bearing
oil film
utility
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 - Lifetime
Application number
CN 200620012192
Other languages
Chinese (zh)
Inventor
何洪
张继忠
王晋伟
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.)
Ningbo Weifu Tianli Turbocharging Technology Co., Ltd.
Original Assignee
No70 Research Institute Of China North Industries Group Corp
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 No70 Research Institute Of China North Industries Group Corp filed Critical No70 Research Institute Of China North Industries Group Corp
Priority to CN 200620012192 priority Critical patent/CN2900796Y/en
Application granted granted Critical
Publication of CN2900796Y publication Critical patent/CN2900796Y/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/23Gas turbine engines
    • F16C2360/24Turbochargers

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  • Supercharger (AREA)

Abstract

The utility model discloses a turbocharger anti-thrust bearing belonging to motive power machine technology. The utility model is characterized in that the turbocharger anti-thrust bearing comprises eight bearing blocks equispacing in a circle around the bearing, the blocks comprises an oil wedge bevel, block plans and oil grooves. The oil wedge bevel is arranged between the oil grooves and the block plans. The utility model greatly improves the bearing capacity of the bearing.

Description

A kind of thrust bearing of turbocharger
Technical field: the utility model belongs to the technical field of bearings of dynamic power machine, is specifically related to a kind of thrust bearing of turbocharger.
Background technique: under the vehicular engine operating mode, for the pressurized machine of mesohigh ratio, the pressure range of supercharger air compressor and turbine is higher, and in the high pressure-charging and super high pressure-charging pressurized machine that are applicable to than high power engine, this point performance is particularly outstanding.The high dynamic change of the pressure of supercharger air compressor and turbine, caused the booster thrust bearing produced bigger thrust loading of having born, this will make a very bad impression to the mechanical efficiency and the thrust-bearing reliability of pressurized machine, on several pressurized machines, just thrust bearing load-carrying properties problem had once appearred, the thrust bearing wearing and tearing are very serious, and bearing capacity is low.
The model utility content: the utility model is just in order to solve the deficiencies in the prior art, and proposes a kind of thrust bearing of turbocharger.
The technical solution of the utility model is: a kind of thrust bearing of turbocharger, thrust bearing is made up of 8 bearing tiles that are uniformly distributed along the circumference, bearing tile is made up of oil film wedge inclined-plane, bearing tile plane and oil groove, and the oil film wedge inclined-plane is in the middle of oil groove and bearing tile plane.
The purpose of this utility model can also be further perfect by following steps: the oil film wedge on oil film wedge inclined-plane is 0.05-0.1mm deeply, cornerite is respectively 4/5 and 3/5 of bearing tile cornerite, the inclined-plane on oil film wedge inclined-plane is a space curved surface, and its border is surrounded by two sections circular arcs and two sections straight lines of crossing the center of circle.
The beneficial effects of the utility model: the plane thrust bearing is adopted in some design at present, the defective of this bearing is that bearing capacity is extremely low, plane bearing is difficult to obtain advantages of high bearing capacity under the normal clearance condition, as oil slick thickness 15 microns the time, bearing capacity is 510 newton, and the thrust bearing bearing capacity that improves design is 4680 newton, is 9.2 times of plane bearing scheme.
Description of drawings: the utility model has 2 width of cloth accompanying drawings, and wherein Fig. 1 is a most preferred embodiment of the present utility model, also can make the specification digest accompanying drawing.
Fig. 1, be structural representation of the present utility model;
Fig. 2, be that the A-A of Fig. 1 is to sectional view.
Embodiment: most preferred embodiment of the present utility model is described further below in conjunction with accompanying drawing:
Most preferred embodiment of the present utility model as shown in Figure 1, 2, a kind of thrust bearing of turbocharger, thrust bearing 1 is made up of 8 bearing tiles that are uniformly distributed along the circumference, bearing tile is made up of oil film wedge inclined-plane 2, bearing tile plane 3 and oil groove 4, and oil film wedge inclined-plane 2 is in the middle of oil groove 4 and bearing tile plane 3.The oil film wedge on oil film wedge inclined-plane 2 is 0.05-0.1mm deeply, cornerite along circumference is respectively 4/5 and 3/5 of bearing tile cornerite, the inclined-plane on oil film wedge inclined-plane 2 is space curved surfaces, and its border is surrounded by two sections circular arcs and two sections straight lines of crossing the center of circle, and the remaining part of bearing tile is made up of bearing tile plane 3.The thrust bearing internal diameter is 20 millimeters; The thrust bearing external diameter is 40 millimeters.
Thrust bearing 1 is installed on the turbosupercharger, and thrust bearing 1 is pressed on the bearing support by back of the body dish or screw, and oil supply gallery communicates with the bearing support oil supply gallery, and two thrust plates are by the running shaft driven rotary, and thrust bearing 1 maintains static.

Claims (2)

1, a kind of thrust bearing of turbocharger, thrust bearing (1) is made up of 8 bearing tiles that are uniformly distributed along the circumference, it is characterized in that: bearing tile is made up of oil film wedge inclined-plane (2), bearing tile plane (3) and oil groove (4), has oil film wedge (2) in the middle of oil groove (4) and bearing tile plane (3).
2, a kind of thrust bearing of turbocharger according to claim 1, thrust bearing (1) is made up of 8 bearing tiles that are uniformly distributed along the circumference, it is characterized in that: the oil film wedge on said oil film wedge inclined-plane (2) is 0.05-0.1mm deeply, cornerite is respectively 4/5 and 3/5 of bearing tile cornerite, the inclined-plane on oil film wedge inclined-plane (2) is a space curved surface, and its border is surrounded by two sections circular arcs and two sections straight lines of crossing the center of circle.
CN 200620012192 2006-04-27 2006-04-27 Thrust bearing of turbocharger Expired - Lifetime CN2900796Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200620012192 CN2900796Y (en) 2006-04-27 2006-04-27 Thrust bearing of turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200620012192 CN2900796Y (en) 2006-04-27 2006-04-27 Thrust bearing of turbocharger

Publications (1)

Publication Number Publication Date
CN2900796Y true CN2900796Y (en) 2007-05-16

Family

ID=38084961

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200620012192 Expired - Lifetime CN2900796Y (en) 2006-04-27 2006-04-27 Thrust bearing of turbocharger

Country Status (1)

Country Link
CN (1) CN2900796Y (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105689545A (en) * 2016-02-01 2016-06-22 上海良基博方汽车发动机零部件制造股份有限公司 Rapid processing device of thrust bearing bevel oil groove of turbocharger
CN106089330A (en) * 2015-04-30 2016-11-09 通用汽车环球科技运作有限责任公司 2 grades of slope thrust bearing base designs under fog lubrication situation
CN107327475A (en) * 2017-07-13 2017-11-07 北京航空航天大学 A kind of floating type thrust bearing of damping greatly of anti-high pulsation
CN109611448A (en) * 2018-12-21 2019-04-12 成都利君实业股份有限公司 A kind of adjusting center sliding bearing

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106089330A (en) * 2015-04-30 2016-11-09 通用汽车环球科技运作有限责任公司 2 grades of slope thrust bearing base designs under fog lubrication situation
CN105689545A (en) * 2016-02-01 2016-06-22 上海良基博方汽车发动机零部件制造股份有限公司 Rapid processing device of thrust bearing bevel oil groove of turbocharger
CN107327475A (en) * 2017-07-13 2017-11-07 北京航空航天大学 A kind of floating type thrust bearing of damping greatly of anti-high pulsation
CN107327475B (en) * 2017-07-13 2019-08-09 北京航空航天大学 A kind of floating type thrust bearing of damping greatly of anti-high pulsation
CN109611448A (en) * 2018-12-21 2019-04-12 成都利君实业股份有限公司 A kind of adjusting center sliding bearing
CN109611448B (en) * 2018-12-21 2023-11-14 成都利君实业股份有限公司 But aligning slide bearing

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: NINGBO TIANLI SUPERCHARGER CO., LTD.

Free format text: FORMER OWNER: NO.70 INST., CHINA WEAPON INDUSTRY GROUP

Effective date: 20080822

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20080822

Address after: Zhejiang province Ningbo City Jiangbei District Haichuan Road 168 Lane 1, zip code: 315000

Patentee after: Ningbo Tianli Turbocharger Co., Ltd.

Address before: Box 22, Shanxi, Datong Province, zip code: 037036

Patentee before: No.70 Research Institute of China North Industries Group Corp.

C56 Change in the name or address of the patentee

Owner name: NINGBO WEIFU TIANLI TURBOCHARGING TECHNOLOGY CO.,

Free format text: FORMER NAME: NINGBO TIANLI TURBOCHARGER CO., LTD.

CP03 Change of name, title or address

Address after: 315032 Zhejiang Province, Ningbo Jiangbei District Haichuan Road 168 Lane No. 1

Patentee after: Ningbo Weifu Tianli Turbocharging Technology Co., Ltd.

Address before: 315000 Zhejiang Province, Ningbo Jiangbei District Haichuan Road 168 Lane No. 1

Patentee before: Ningbo Tianli Turbocharger Co., Ltd.

CX01 Expiry of patent term

Granted publication date: 20070516

EXPY Termination of patent right or utility model