CN107588039A - A kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger - Google Patents

A kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger Download PDF

Info

Publication number
CN107588039A
CN107588039A CN201711012043.1A CN201711012043A CN107588039A CN 107588039 A CN107588039 A CN 107588039A CN 201711012043 A CN201711012043 A CN 201711012043A CN 107588039 A CN107588039 A CN 107588039A
Authority
CN
China
Prior art keywords
cover plate
boss
radial direction
chimb
pressure side
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.)
Granted
Application number
CN201711012043.1A
Other languages
Chinese (zh)
Other versions
CN107588039B (en
Inventor
范厚传
曲大勇
郑义
郎宏兵
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.)
Fengcheng City Shidailong Supercharger Manufacturing Co Ltd
Original Assignee
Fengcheng City Shidailong Supercharger Manufacturing Co 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 Fengcheng City Shidailong Supercharger Manufacturing Co Ltd filed Critical Fengcheng City Shidailong Supercharger Manufacturing Co Ltd
Priority to CN201711012043.1A priority Critical patent/CN107588039B/en
Publication of CN107588039A publication Critical patent/CN107588039A/en
Application granted granted Critical
Publication of CN107588039B publication Critical patent/CN107588039B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Supercharger (AREA)

Abstract

Calmed the anger the sealing structure of generator terminal for ball bearing turbine supercharger the present invention relates to a kind of.Technical scheme is:Including sealing axle sleeve, oil pocket cover plate and pressure side sealing ring, closure gasket groove and radial direction boss are provided with sealing axle sleeve, radial direction boss is provided with bearing end axial direction chimb and pressure side axial direction chimb, bearing end axial direction chimb forms bearing end groove with radial direction boss, and pressure side axial direction chimb forms pressure side groove with radial direction boss;Oil pocket cover plate is provided with cover plate axial boss and edge lug boss, the radial component of cover plate axial boss and edge lug boss and oil pocket cover plate collectively forms cover plate axial notch, cover plate axial boss is provided with cover plate radial direction chimb, and the radial component of cover plate radial direction chimb and cover plate axial boss and oil pocket cover plate collectively forms cover plate radial groove;Cover plate radial direction chimb is placed in pressure side groove, and pressure side sealing ring is provided between sealing axle sleeve and oil pocket cover plate.Lubricating oil in the intermediate oil pocket of the invention for having the function that to completely cut off turbocharger.

Description

A kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger
Technical field
The invention belongs to internal combustion engine turbocharging technical field, and in particular to one kind is calmed the anger for ball bearing turbine supercharger The sealing structure of generator terminal.
Background technology
The purpose of turbocharging technology is to improve the fuel economy of engine, power performance, can reduce engine emission, Performance on Plateau that is Engine Downsizing, and compensating vehicular engine can be made.Turbocharger not consumption of engine it is effective Power, the exhaust energy that its turbine discharges engine reclaim, and drive coaxial compressor pressurised fresh air, so as to increase hair The air inflow of motivation, increase the power density of engine.
The bearing of turbocharger experienced the developing stage of sliding bearing, floating bearing and ball bearing, and ball bearing is to increase The newest bearing arrangement of depressor.Compared to the booster of application floating bearing, booster can simplify supercharging after using ball bearing Device structure, thrust bearing, thrust housing and gear oil that conventional float bearing booster is possessed are fitted without on ball bearing booster Plate.
The one-piece corner connection that ball bearing booster is installed by it, which touches ball bearing, can balance the axial force of booster.Ball The generator terminal of calming the anger of bearing booster is also equipped with pressure side seal ring structure and is used to separate compressor and intermediate oil pocket, still, by There is no special oil baffle in ball bearing booster, and pressure side sealing ring junction seal and oil-blocking action on ball bearing booster It is limited, this just needs to focus on devising for sealing axle sleeve and oil pocket cover plate, it is necessary to matching somebody with somebody sealing axle sleeve and oil pocket cover plate Conjunction face is designed to be able to gear oil, has the function that to completely cut off lubricating oil in intermediate oil pocket.
At present, ball bearing research and application do not carry out on a large scale also, the design and research of its sealing system do not have In depth carry out.
The content of the invention
The present invention provides a kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger, has isolation turbocharging The effect of lubricating oil in the intermediate oil pocket of device.
Technical scheme is as follows:
A kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger, including sealing axle sleeve, oil pocket cover plate and pressure Sealing ring is held, closure gasket groove and radial direction boss are provided with the sealing axle sleeve, the radial direction boss is provided with bearing end axial direction Chimb and pressure side axial direction chimb, bearing end axial direction chimb form bearing end groove with radial direction boss, and the pressure side is axially convex Side forms pressure side groove with radial direction boss;The oil pocket cover plate is provided with cover plate axial boss and edge lug boss, the plate shaft Cover plate axial notch is collectively formed to the radial component of boss and edge lug boss and oil pocket cover plate, is set in the cover plate axial boss There is cover plate radial direction chimb, the cover plate radial direction chimb and the radial component of the cover plate axial boss and oil pocket cover plate collectively form Cover plate radial groove;The internal diameter of pressure side axial direction chimb is more than the external diameter of the cover plate radial direction chimb, the cover plate radial convex While being placed in the pressure side groove, the pressure side sealing ring is provided between sealing axle sleeve and the oil pocket cover plate.The sealing Structure setting is on the armature spindle of turbocharger, between compressor impeller and ball bearing.
Beneficial effects of the present invention are:Radial direction boss, pressure side axial direction chimb and the bearing end axial direction chimb of sealing axle sleeve, with And the cover plate radial direction chimb of oil pocket cover plate collectively constitutes oil baffle structure with cover plate axial boss so that flows to and presses from intermediate oil pocket The lubricating oil at mechanism of qi end is blocked in intermediate one end, it is impossible to smoothly enters pressure side sealing ring position, lubricating oil passes through seal shaft The bearing end groove of set and the cover plate axial notch of oil pocket cover plate flow to the oil return opening of intermediate with cover plate radial groove.This gear oil Structure coordinates pressure side seal ring structure again, can effectively obstruct lubricating oil and enter generator terminal of calming the anger.
Brief description of the drawings
Fig. 1 is the structure chart using the ball bearing turbine supercharger of sealing structure of the present invention;
Fig. 2 is the structural representation of sealing structure of the present invention;
Fig. 3 is the structure chart of sealing axle sleeve;
Fig. 4 is the structure chart of oil pocket cover plate;
Marked in figure:
1st, sealing axle sleeve, 101, radial direction boss, 102, bearing end axial direction chimb, 103, bearing end groove, 104, pressure side axle To chimb, 105, pressure side groove, 106, closure gasket groove, 2, oil pocket cover plate, 201, cover plate radial groove, 202, cover plate radial convex Side, 203, cover plate axial boss, 204, cover plate axial notch, 3, ball bearing, 4, armature spindle, 5, compressor impeller, 6, intermediate, 7th, compressor casing, 8, pressure side sealing ring.
Embodiment
As Figure 1-4, ball bearing turbine supercharger includes compressor, turbine, intermediate 6, ball bearing 3, armature spindle 4th, compressor impeller 5 and sealing structure.Sealing structure includes sealing axle sleeve 1, oil pocket cover plate 2 and pressure side sealing ring 8, the sealing Closure gasket groove 106 and radial direction boss 101 are provided with axle sleeve 1, the radial direction boss 101 is provided with bearing end axial direction chimb 102 With pressure side axial direction chimb 104, bearing end axial direction chimb 102 forms bearing end groove 103, the pressure with radial direction boss 101 Axial chimb 104 is held to form pressure side groove 105 with radial direction boss 101;The oil pocket cover plate 2 is provided with cover plate axial boss 203 And the radial component of edge lug boss, the cover plate axial boss 203 and edge lug boss and oil pocket cover plate collectively forms cover plate axial direction Groove 204, the cover plate axial boss 203 are provided with cover plate radial direction chimb 202, the cover plate radial direction chimb 202 and the lid The radial component of plate axial boss 203 and oil pocket cover plate collectively forms cover plate radial groove 201;Pressure side axial direction chimb 104 Internal diameter be more than the external diameter of the cover plate radial direction chimb 202, the cover plate radial direction chimb 202 is placed on the pressure side groove 105 In, the pressure side sealing ring 8 is provided between the sealing axle sleeve 1 and oil pocket cover plate 2.The sealing structure is arranged on turbocharging On the armature spindle 4 of device, between compressor impeller 5 and ball bearing 3.
During work, the lubricating oil come from the oil pocket stream of intermediate 6 is by the bearing end groove 103 and bearing end of sealing axle sleeve 1 Axial chimb 102 keeps off back the oil return opening of intermediate 6, and the lubricating oil not being blocked is by cover plate radial groove 201 and cover plate radial convex Side 202 is blocked, and the oil return opening of intermediate 6 is then flowed to by cover plate axial notch 204.
Above is the explanation that we are carried out according to national patent method to the present invention, present invention specific implementation is not limited to State bright;The improvement or replacement of specific embodiment disclosed in this invention can be identified for related personnel in the art, is Within the spirit and scope of the present invention.

Claims (2)

1. a kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger, it is characterised in that including sealing axle sleeve, oil pocket Cover plate and pressure side sealing ring, closure gasket groove and radial direction boss are provided with the sealing axle sleeve, the radial direction boss is provided with axle Socket end axial direction chimb and pressure side axial direction chimb, bearing end axial direction chimb form bearing end groove, the pressure with radial direction boss Axial chimb is held to form pressure side groove with radial direction boss;The oil pocket cover plate is provided with cover plate axial boss and edge lug boss, institute The radial component for stating cover plate axial boss and edge lug boss and oil pocket cover plate collectively forms cover plate axial notch, the cover plate axial direction Boss is provided with cover plate radial direction chimb, the cover plate radial direction chimb and the cover plate axial boss and the radial component of oil pocket cover plate Collectively form cover plate radial groove;The internal diameter of pressure side axial direction chimb is more than the external diameter of the cover plate radial direction chimb, the lid Plate radial direction chimb is placed in the pressure side groove, and the pressure side sealing ring is provided between sealing axle sleeve and the oil pocket cover plate.
2. the sealing structure of generator terminal according to claim 1 of being calmed the anger for ball bearing turbine supercharger, it is characterised in that set Put on the armature spindle of turbocharger, between compressor impeller and ball bearing.
CN201711012043.1A 2017-10-26 2017-10-26 Sealing structure for compressor end of ball bearing turbocharger Active CN107588039B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711012043.1A CN107588039B (en) 2017-10-26 2017-10-26 Sealing structure for compressor end of ball bearing turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711012043.1A CN107588039B (en) 2017-10-26 2017-10-26 Sealing structure for compressor end of ball bearing turbocharger

Publications (2)

Publication Number Publication Date
CN107588039A true CN107588039A (en) 2018-01-16
CN107588039B CN107588039B (en) 2024-03-05

Family

ID=61045336

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711012043.1A Active CN107588039B (en) 2017-10-26 2017-10-26 Sealing structure for compressor end of ball bearing turbocharger

Country Status (1)

Country Link
CN (1) CN107588039B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101509399A (en) * 2008-12-18 2009-08-19 寿光市康跃增压器有限公司 Split axial carrying device of turbo-charger
CN203404120U (en) * 2013-06-28 2014-01-22 湖南天雁机械有限责任公司 Sealing structure of turbocharger compressor
CN203685664U (en) * 2014-01-22 2014-07-02 重庆江增机械有限公司 Turbocharger compressor combination sealing structure
CN105863827A (en) * 2016-06-08 2016-08-17 湖南天雁机械有限责任公司 Sealing structure and method for pressure end and vortex end of ball bearing turbocharger
CN106194818A (en) * 2016-08-31 2016-12-07 中车大连机车研究所有限公司 Centrifugal-flow compressor novel pressure side oil-gas seal structure
CN107288741A (en) * 2017-06-24 2017-10-24 凤城市时代龙增压器制造有限公司 A kind of band gets rid of the turbocharger of tank structure
CN207377856U (en) * 2017-10-26 2018-05-18 凤城市时代龙增压器制造有限公司 A kind of sealing structure for generator terminal of calming the anger for ball bearing turbine supercharger

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101509399A (en) * 2008-12-18 2009-08-19 寿光市康跃增压器有限公司 Split axial carrying device of turbo-charger
CN203404120U (en) * 2013-06-28 2014-01-22 湖南天雁机械有限责任公司 Sealing structure of turbocharger compressor
CN203685664U (en) * 2014-01-22 2014-07-02 重庆江增机械有限公司 Turbocharger compressor combination sealing structure
CN105863827A (en) * 2016-06-08 2016-08-17 湖南天雁机械有限责任公司 Sealing structure and method for pressure end and vortex end of ball bearing turbocharger
CN106194818A (en) * 2016-08-31 2016-12-07 中车大连机车研究所有限公司 Centrifugal-flow compressor novel pressure side oil-gas seal structure
CN107288741A (en) * 2017-06-24 2017-10-24 凤城市时代龙增压器制造有限公司 A kind of band gets rid of the turbocharger of tank structure
CN207377856U (en) * 2017-10-26 2018-05-18 凤城市时代龙增压器制造有限公司 A kind of sealing structure for generator terminal of calming the anger for ball bearing turbine supercharger

Also Published As

Publication number Publication date
CN107588039B (en) 2024-03-05

Similar Documents

Publication Publication Date Title
CN201627605U (en) Sealing and heat insulation structure at vortex end of turbocharger
CN106837528B (en) Sequential supercharged diesel engine lubrication sealing structure and its control method based on tonifying Qi
CN207377856U (en) A kind of sealing structure for generator terminal of calming the anger for ball bearing turbine supercharger
CN101975185A (en) Compressor seal structure of small turbocharger
CN107588039A (en) A kind of sealing structure for generator terminal of being calmed the anger for ball bearing turbine supercharger
CN203515788U (en) Air feeding and supercharging device of gas engine
CN201062538Y (en) Propeller shaft and tube for leak-proof turbocharger bypass valve
CN103912577A (en) Split-type turbocharger thrust bearing
CN217055298U (en) Shaft end sealing structure of turbocharger
CN201297201Y (en) Oil-leak resisting turbocharger
CN103398095A (en) Thrust bearing and engine supercharger having the same
CN101344033A (en) Transmission shaft and shaft sleeve of anti-air leakage turbosupercharger bypass valve
CN206487553U (en) Turbocharger of motor oil return pipe
CN202578937U (en) Crankcase cover of internal combustion engine
CN203756726U (en) Split-type turbosupercharger thrust bearing
CN108533387A (en) A kind of turbo charging installation of translator/generator
CN209129685U (en) Variable-geometry mixed-flow turbocharger sealing structure
CN203321669U (en) Turbocharger intermediate
CN201581982U (en) Air bearing of turbocharger
CN204646413U (en) Exhaust-gas turbocharger gas compressor end sealing configuration
CN203500276U (en) Thrust bearing and engine supercharger having same
CN201844022U (en) Seal structure of compressor of small turbocharger
CN204729351U (en) A kind of compressor housings of modified model turbosupercharger
CN202441885U (en) Sealing device for compressor end of turbocharger
CN219865234U (en) Cooling system for rotor engine moving parts

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant