CN207539073U - A kind of novel rotor axis - Google Patents
A kind of novel rotor axis Download PDFInfo
- Publication number
- CN207539073U CN207539073U CN201721599843.3U CN201721599843U CN207539073U CN 207539073 U CN207539073 U CN 207539073U CN 201721599843 U CN201721599843 U CN 201721599843U CN 207539073 U CN207539073 U CN 207539073U
- Authority
- CN
- China
- Prior art keywords
- linkage section
- rotor axis
- seal groove
- novel rotor
- impeller
- 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
Links
Landscapes
- Supercharger (AREA)
Abstract
The utility model discloses a kind of novel rotor axis, the component being related in a kind of turbocharger, including turbine linkage section, bearing linkage section, impeller linkage section and the threaded connection section being wholely set successively, cricoid seal groove is offered on the turbine linkage section, several limit protrusions and several limiting slots are circumferentially provided on the both sides cell wall of the seal groove, the limit protrusion is arranged at intervals with limiting slot；The utility model realizes armature spindle and the circumferential direction of sealing ring is limited so that sealing ring be in relative static conditions with armature spindle, reduces the abrasion of sealing ring, prevent to generate gap between sealing ring and seal groove and so that the leakage of lubricating oil.
Description
Technical field
The utility model is related to the component in a kind of turbocharger, more particularly to a kind of novel rotor axis.
Background technology
Turbocharger is that one kind of raising gasoline or diesel internal combustion acc power is attached under conditions of engine displacement is constant
Feeder apparatus, vehicle turbocharger are mainly made of compressor, turbine and intermediate three parts.Armature spindle is threaded onto supercharging
In device, turbine of the both ends respectively with the impeller of compressor and turbine is fixedly connected, and is passed through two floating bearings and be supported on
In intermediate, the oil duct of lubrication and cooling bearing is equipped in intermediate, usual armature spindle offers at the position of installation turbine
Cricoid seal groove, sealing shroud be mounted on seal groove in and it is opposing stationary with armature spindle, with prevent the lubricating oil in oil duct along
The outer wall of armature spindle is leaked out on turbine.
For turbocharger in actual moving process, turbine rotation drives armature spindle rotation, armature spindle high-speed rotating wink
Between sealing shroud still in stationary state so that relatively rotate between sealing shroud and armature spindle, in the process of long-time service
Middle sealing ring and armature spindle can generate certain abrasion, and then cause to generate gap between sealing shroud and armature spindle, in intermediate
Lubricating oil the rotation of turbine can be leaked out in turbine and influenced along the gap between sealing shroud and armature spindle.
Utility model content
The purpose of this utility model is to provide a kind of novel rotor axis, and which solve armature spindles of the prior art and sealing
Set relatively rotates so that leading to the problem of gap between the two and causing oil leak.
The above-mentioned technical purpose of the utility model technical scheme is that：
A kind of novel rotor axis, including be wholely set successively turbine linkage section, bearing linkage section, impeller linkage section and
Threaded connection section, offers cricoid seal groove on the turbine linkage section, circumferentially disposed on the both sides cell wall of the seal groove
There are several limit protrusions and several limiting slots, the limit protrusion is arranged at intervals with limiting slot.
Using the above scheme, when in use, turbine is installed on turbine linkage section armature spindle, and bearing linkage section passes through floating
Bearing is maked somebody a mere figurehead in intermediate, and impeller is usually installed on using clamp spring on impeller linkage section, and threaded connection section is used for reinforcing clip
The fixation of spring, sealing shroud are installed in seal groove, and limit protrusion and limiting slot prevent relatively to turn between seal groove and sealing ring
It is dynamic, to realize that armature spindle limits the circumferential direction of sealing ring so that sealing ring is in relative static conditions with armature spindle, reduces close
The abrasion of seal avoids generating the leakage that gap causes lubricating oil between sealing ring and seal groove.
Further preferably：The side of cell wall of the limit protrusion far from the seal groove is opened up there are one groove.
Using the above scheme, temperature is higher in the process of running for usual booster, the sealing shroud meeting being installed on armature spindle
Certain elastic deformation occurs and fills into groove, strengthens armature spindle and the circumferential direction of sealing shroud is limited.
Further preferably：Limit protrusion on the cell wall of the seal groove side and the limit on seal groove opposite side cell wall
Position slot is oppositely arranged.
Using the above scheme, when sealing shroud is installed in limiting slot, limit protrusion compresses axially sealing shroud to limit
In the slot of position, so that sealing shroud is in bending on the circumferential surface of armature spindle, and then with good circumferential position-limiting action.
Further preferably：The limit protrusion is spherical in semicircle.
Using the above scheme, the Surface of Sphere of limit protrusion plays guiding role when sealing shroud is installed, convenient for sealing shroud
Fast Installation.
Further preferably：The limit protrusion is in strip, and the length direction of limit protrusion is connected for the turbine
The diametric(al) of section.
Using the above scheme, the limit protrusion of strip is relatively large to the forced area of sealing shroud so that protrusion is given
The active force of sealing shroud is uniformly distributed, and has good circumferential position-limiting action.
Further preferably：There are two the seal groove is arranged in parallel.
Using the above scheme, two seal grooves increase the approach of oil seepage relative to single seal groove, improve
Turbocharger reduces production cost in the leakproofness of turbine linkage section relative to other multiple seal grooves, has good
Practicability.
Further preferably：The impeller linkage section and the junction of the threaded connection section are provided with the first guide surface,
The one end of the threaded connection section far from impeller linkage section is provided with the second guide surface.
Using the above scheme, the first guide surface and the second guide surface play guiding role to impeller, convenient for accelerating impeller
Installation.
Further preferably：The impeller linkage section is provided with form friction pattern ring on the circumferential surface by close end.
Using the above scheme, impeller is mounted on impeller linkage section, and form friction pattern ring strengthens impeller and impeller linkage section
Connection.
Further preferably：It is both provided on the circumferential surface of the turbine linkage section, bearing linkage section and impeller linkage section
Wear-resistant coating.
Using the above scheme, the setting of wear-resistant coating slows down the abrasion of armature spindle, and then increase turbine linkage section
Usage time.
In conclusion the utility model has the advantages that：
1st, it by the setting of limit protrusion, limiting slot and groove, realizes armature spindle and the circumferential direction of sealing ring is limited, make
It obtains sealing ring and is in relative static conditions with armature spindle, reduce the abrasion of sealing ring, prevent to produce between sealing ring and seal groove
Raw gap causes the leakage of lubricating oil；
2nd, by the setting of wear-resistant coating, the abrasion of armature spindle is slowed down, extends the usage time of armature spindle；
3rd, it by the setting of the first guide surface and form friction pattern ring, convenient for the Fast Installation of impeller, increases impeller and is mounted on
Structural stability on armature spindle.
Description of the drawings
Fig. 1 is the structure diagram of embodiment one；
Fig. 2 is the structure diagram of the worm gear linkage section of embodiment one；
Fig. 3 is the structure diagram of embodiment two；
Fig. 4 is the structure diagram of the worm gear linkage section of embodiment two.
In figure, 1, turbine linkage section；2nd, bearing linkage section；3rd, impeller linkage section；4th, threaded connection section；11st, seal groove；
111st, limit protrusion；1111st, groove；112nd, limiting slot；31st, the first guide surface；32nd, form friction pattern ring；41st, the second guide surface.
Specific embodiment
The utility model is described in further detail below in conjunction with attached drawing.
Embodiment one：
A kind of novel rotor axis, as shown in Figure 1, including the turbine linkage section 1, bearing linkage section 2, leaf that are wholely set successively
Take turns linkage section 3 and threaded connection section 4.Wherein, on the circumferential surface of turbine linkage section 1, bearing linkage section 2 and impeller linkage section 3
It is both provided with the wear-resistant coating being laid with by ceramic layer（It is not shown in figure）.
As depicted in figs. 1 and 2, the diameter of turbine linkage section 1 is less than the diameter of bearing linkage section 2, is put down on turbine linkage section 1
Row is opened up there are two cricoid seal groove 11, and being circumferentially provided with for the both sides cell wall upper edge turbine linkage section 1 of seal groove 11 is several
Limit protrusion 111 and several limiting slots 112.Wherein, limit protrusion 111 and limiting slot 112 are spherical in semicircle, and seal groove 11
Limit protrusion 111 on the cell wall of the same side is set with 112 uniform intervals of limiting slot, the limiting on the wherein side cell wall of seal groove 11
Limiting slot 112 of the protrusion 111 corresponding thereto on the cell wall of side is oppositely arranged.Cell wall of the limit protrusion 111 far from seal groove 11
Side is further opened with a spherical groove of semicircle 1111.
The diameter of impeller linkage section 3 is less than bearing linkage section 2, and the diameter of threaded connection section 4 is less than the straight of impeller linkage section 3
Diameter, and impeller linkage section 3 is provided with the first guide surface 31 in the junction with threaded connection section 4, impeller linkage section 3 is close to it
A form friction pattern ring 32 is respectively arranged on the circumferential surface of two ends, threaded connection section 4 is set in one end far from impeller linkage section 3
It is equipped with the second guide surface 41.
Embodiment two：As shown in Figure 3 and Figure 4, the difference lies in limit protrusion 111 and limiting slots with embodiment one
112 in strip, and the length direction of limit protrusion 111 and limiting slot 112 is the diametric(al) of turbine linkage section 1, and two
The length of person is consistent in the diametric length of turbine linkage section 1 with seal groove 11.
This specific embodiment is only explanation to the utility model, is not the limitation to the utility model, ability
Field technique personnel can as needed make the present embodiment the modification of no creative contribution after this specification is read, but
As long as within the protection scope of the present utility model all protected by Patent Law.
Claims (9)
1. a kind of novel rotor axis, it is characterised in that：Including turbine linkage section (1), the bearing linkage section being wholely set successively
(2), impeller linkage section (3) and threaded connection section (4) offer cricoid seal groove (11) on the turbine linkage section (1),
Several limit protrusions (111) and several limiting slots (112), the limit are circumferentially provided on the both sides cell wall of the seal groove (11)
Position raised (111) is arranged at intervals with limiting slot (112).
2. a kind of novel rotor axis according to claim 1, it is characterised in that：The limit protrusion (111) is far from described
The side of the cell wall of seal groove (11) is opened up there are one groove (1111).
3. a kind of novel rotor axis according to claim 1, it is characterised in that：On the cell wall of seal groove (11) side
Limit protrusion (111) is oppositely arranged with the limiting slot (112) on seal groove (11) opposite side cell wall.
4. a kind of novel rotor axis according to claim 3, it is characterised in that：The limit protrusion (111) is in semi-round ball
Shape.
5. a kind of novel rotor axis according to claim 3, it is characterised in that：The limit protrusion (111) in strip,
And the diametric(al) that the length direction of limit protrusion (111) is the turbine linkage section (1).
6. a kind of novel rotor axis according to claim 4 or 5, it is characterised in that：The seal groove (11) is arranged in parallel
There are two.
7. a kind of novel rotor axis according to claim 1, it is characterised in that：The impeller linkage section (3) and the spiral shell
The junction of line linkage section (4) is provided with the first guide surface (31), the separate impeller linkage section (3) of the threaded connection section (4)
One end is provided with the second guide surface (41).
8. a kind of novel rotor axis according to claim 7, it is characterised in that：The impeller linkage section (3) is by proximal end
Form friction pattern ring (32) is provided on the circumferential surface in portion.
9. a kind of novel rotor axis according to claim 1, it is characterised in that：The turbine linkage section (1), bearing connection
Wear-resistant coating is both provided on the circumferential surface of section (2) and impeller linkage section (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721599843.3U CN207539073U (en) | 2017-11-24 | 2017-11-24 | A kind of novel rotor axis |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721599843.3U CN207539073U (en) | 2017-11-24 | 2017-11-24 | A kind of novel rotor axis |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207539073U true CN207539073U (en) | 2018-06-26 |
Family
ID=62615208
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721599843.3U Expired - Fee Related CN207539073U (en) | 2017-11-24 | 2017-11-24 | A kind of novel rotor axis |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207539073U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108712008A (en) * | 2018-07-06 | 2018-10-26 | 无锡市海星船舶动力有限公司 | Has the armature spindle of multistage aeration structure |
| CN108757545A (en) * | 2018-07-06 | 2018-11-06 | 无锡市海星船舶动力有限公司 | The armature spindle that installation rigidized cover is bonded |
-
2017
- 2017-11-24 CN CN201721599843.3U patent/CN207539073U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108712008A (en) * | 2018-07-06 | 2018-10-26 | 无锡市海星船舶动力有限公司 | Has the armature spindle of multistage aeration structure |
| CN108757545A (en) * | 2018-07-06 | 2018-11-06 | 无锡市海星船舶动力有限公司 | The armature spindle that installation rigidized cover is bonded |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8043012B2 (en) | Seal arrangement and a brush seal for a wind turbine | |
| CN207539073U (en) | A kind of novel rotor axis | |
| CN204511526U (en) | Seal arrangement | |
| CN102762880A (en) | Rolling bearing lubrication structure and rolling bearing | |
| CN101644185A (en) | Hybrid ceramic ball bearing turbine supercharger without inner ring | |
| CN206468449U (en) | Gas turbine rotor sealing graphite seal device and gas turbine | |
| CN202012570U (en) | Oil film bearing of main shaft of wind driven generator | |
| CN203478937U (en) | Spring ejector rod type graphite block sealing device based on rotary kiln | |
| CN201225402Y (en) | Adjustable automatic following and cellular compound oil seal | |
| CN107314114A (en) | A kind of comb tooth sealing structure | |
| CN202364039U (en) | Ceramic-ball three-bearing structure for 5MW double-fed wind turbine generator | |
| CN101550864B (en) | Turbocharger supported by pressure-charging flow passage groove self-lubricating dynamic-static pressure air bearing | |
| CN101975185A (en) | Compressor seal structure of small turbocharger | |
| CN205278110U (en) | Booster bearing arrangement that floats | |
| CN207569053U (en) | A kind of precision electric motor bearing | |
| CN201902291U (en) | Variable-propeller bearing for wind power generation | |
| CN204784726U (en) | Low friction oil blanket | |
| CN204647314U (en) | Seal arrangement | |
| CN203702850U (en) | Ball bearing unit for turbocharger | |
| CN210509989U (en) | Wind power main shaft system with permanent magnetic suspension bearing | |
| CN102022538A (en) | Rotating shaft sealing device | |
| CN204082231U (en) | Separated type high speed scroll turbocharger bearing body | |
| CN208417246U (en) | A kind of low friction water lubrication macromolecule bearing | |
| CN111306301A (en) | Rotary vane type high-temperature high-pressure gas (liquid) elastic contact dynamic sealing device and preparation method | |
| CN206195521U (en) | Permanent magnet motor bearing room structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180626 Termination date: 20191124 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |