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 PDFInfo
- 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
Links
- 238000007789 sealing Methods 0.000 title claims abstract description 44
- 239000003921 oil Substances 0.000 abstract description 32
- 239000010687 lubricating oil Substances 0.000 abstract description 8
- 239000012208 gear oil Substances 0.000 description 3
- 230000001914 calming effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
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
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.
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)
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 |
-
2017
- 2017-10-26 CN CN201711012043.1A patent/CN107588039B/en active Active
Patent Citations (7)
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 |