CN208805317U - A kind of multistage turbine dynamic balance of impeller tooling - Google Patents
A kind of multistage turbine dynamic balance of impeller tooling Download PDFInfo
- Publication number
- CN208805317U CN208805317U CN201821541685.0U CN201821541685U CN208805317U CN 208805317 U CN208805317 U CN 208805317U CN 201821541685 U CN201821541685 U CN 201821541685U CN 208805317 U CN208805317 U CN 208805317U
- Authority
- CN
- China
- Prior art keywords
- ring
- mounting ring
- impeller
- coning sleeve
- dynamic balance
- 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
- Turbine Rotor Nozzle Sealing (AREA)
- Testing Of Balance (AREA)
Abstract
A kind of multistage turbine dynamic balance of impeller tooling, belong to dynamic balancing detection technique field, mandrel uses Double shaft-extension structure, detection ring is set to the middle part of mandrel, left support, right support is located in the left and right ends of mandrel, left mounting ring is followed successively by between detection ring and left support, left dead ring, right mounting ring is followed successively by between detection ring and right support, right dead ring, left mounting ring, the diameter of right mounting ring successively decreases tapered structure from inside to outside respectively, left mounting ring, left coning sleeve is arranged in socket respectively in right mounting ring, right coning sleeve, left dead ring, helicitic texture is respectively adopted in the outer surface of right dead ring；This patent conceptual design novelty, reasonable idea, using Double shaft-extension and tapered configuration, so that multistage turbine dynamic balance of impeller tooling can be well adapted for the dynamic balance of impeller test of different length, different inner holes in use, assembly technology is simple, it is versatile, cost of labor can be reduced, and the working efficiency of dynamic balance check can be significantly improved.
Description
Technical field
The utility model belongs to rotor dynamic balancing technical field, and in particular to a kind of multistage turbine vacuum pump impeller it is dynamic flat
Weigh tooling.
Background technique
The high speed rotor of several impeller serials is the core component of multistage turbine vacuum pump, and quick runner is generally in asymmetric
Shape design is responsible for the vibration of high speed rotor in addition the error, the material that generate in manufacture process are uneven etc. by element
Dynamic, long-play can cause equipment performance to fluctuate, and reduce the service life of sliding bearing, and lead to equipment fault, therefore right
Impeller carries out dynamic balance check one by one, is a significant process indispensable in multistage turbine vacuum pump device fabrication.
When existing dynamic balancing detection is implemented, every multistage turbine vacuum pump impeller needs specific aim to be equipped with special tooling, with
Performance parameter is continuously increased, and the outer dimension of impeller especially axis hole model is more and more, and original dynamic balancing tooling is equipped with mould
Formula cannot meet production because its versatility is lower in time.In addition, turbine vacuum pump performance develops toward Trend Analysis When Observation Points Are Too Many direction, impeller
Axial length increase, original tooling is time-consuming and laborious when in use, operability it is poor.
Utility model content
The utility model is intended to the connected applications based on Double shaft-extension and tapered configuration, and it is dynamic flat to provide a kind of multistage turbine impeller
Weigh tooling technical solution, and to overcome, the tooling model in the presence of the above-mentioned prior art is complicated, versatility is low, poor operability
The problems such as.
A kind of multistage turbine dynamic balance of impeller tooling, it is special comprising detection ring and left support, right support on mandrel
Sign is the mandrel using Double shaft-extension structure, and detection ring is set to the middle part of mandrel, left support, right support be located in
The left and right ends of mandrel are detected and are followed successively by left mounting ring, left dead ring between ring and left support, detect between ring and right support according to
Secondary is right mounting ring, right dead ring, left mounting ring, right mounting ring diameter successively decrease from inside to outside respectively tapered structure, Zuo An
Fill ring, socket is arranged left coning sleeve, right coning sleeve respectively in right mounting ring, left dead ring, right dead ring outer surface adopt respectively
Use helicitic texture.
A kind of multistage turbine dynamic balance of impeller tooling, it is characterised in that the left coning sleeve, right coning sleeve point
Not Cai Yong circumferencial direction setting notch open loop structure.
A kind of multistage turbine dynamic balance of impeller tooling, it is characterised in that the left coning sleeve, right coning sleeve it is interior
Hole taper is consistent with corresponding left mounting ring, the taper of right mounting ring, and left coning sleeve, the axial length of right coning sleeve are left less than corresponding
The length of mounting ring, right mounting ring, detection ring both sides of the face constitute the positioning step of tested impeller.
A kind of multistage turbine dynamic balance of impeller tooling, it is characterised in that on the left dead ring, right dead ring
It is separately connected left locking nut group, the right locking nut group of setting with its threaded.
The multistage turbine dynamic balance of impeller Fixture Design is novel, reasonable idea is made using Double shaft-extension and tapered configuration
Obtain the dynamic balance of impeller that multistage turbo wheel dynamic balancing tooling can be well adapted for different length, different inner holes in use
Test, assembly technology is simple, versatile, can reduce cost of labor, and can significantly improve the working efficiency of dynamic balance check, protects
Demonstrate,prove equipment performance.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the structural schematic diagram of the left coning sleeve, right coning sleeve；
Fig. 3 is the dynamic balancing detection schematic diagram using the utility model
In figure: 1- mandrel, 1a- left support, the left dead ring of 1b-, the left mounting ring of 1c-, 1d- detect ring, the right peace of 1e-
Fill ring, the right dead ring of 1f-, 1g- right support, the left coning sleeve of 2-, the right coning sleeve of 3-, the left locking nut group of 4-, the right lock of 5-
Tight nut group, 6- positioning step, 7- clump weight, 8- are tested impeller.
Specific embodiment
Now in conjunction with Figure of description, specific embodiment of the present utility model is described in detail:
It as shown is a kind of multistage turbine dynamic balance of impeller tooling, mandrel 1 uses Double shaft-extension structure, and middle part is detection
Ring 1d is used to install the detection device of dynamic balancing machine, and left and right ends are respectively set to left support 1a, right support 1g, left support 1a,
Right support 1g is in contact with the support wheel of dynamic balancing machine plays a supporting role respectively；It is followed successively by between detection ring 1d and left support 1a
Left mounting ring 1c, left dead ring 1b are detected and are followed successively by right mounting ring 1e, right dead ring 1f, Zuo An between ring 1d and right support 1g
Dress ring 1c, right mounting ring 1e diameter successively decrease from inside to outside respectively tapered structure, the diameter of section with detection ring 1d abutting end
It is maximum；Left coning sleeve 2, right coning sleeve 3, left coning sleeve 2, right taper is arranged in socket respectively on left mounting ring 1c, right mounting ring 1e
The hole taper of set 3 is consistent with corresponding left mounting ring 1c, the taper of right mounting ring 1e, the axial direction of left coning sleeve 2, right coning sleeve 3
Length is less than the length of corresponding left mounting ring 1c, right mounting ring 1e, and detection ring 1d both sides of the face constitute the positioning step 6 of impeller；
Left coning sleeve 2, right coning sleeve 3 are respectively used to be socketed tested impeller 8, using the open loop structure of circumferencial direction setting notch, outer circle
Size is according to the bore design for being tested impeller 8；Left dead ring 1b, right dead ring 1f outer surface helicitic texture is respectively adopted and sets
Set with the left locking nut group 4 of its threaded, right locking nut group 5, each locking nut group is respectively by two same sizes
Locking nut composition can prevent tested 8 axial play of impeller, left locking screw using two locking nuts when assembling tested impeller 8
Mother's group 4, right locking nut group 5 can be designed to same size size to improve versatility；When dynamic balancing detection is implemented, left locking
One group in nut group 4, right locking nut group 5 contacts cooperation for fixed tested impeller 8, another group of cooperation with tested impeller 8
Clump weight 7 is set, inner screw nut in locking nut group can be replaced as to clump weight 7, outboard nut is for fixing in practical application
Clump weight 7.
In above-described embodiment, left coning sleeve 2, right coning sleeve 3 are adapted to the tested impeller 8 of different model and specification, left cone
Degree set 2, right coning sleeve 3 have the notch of appropriate width in circumferencial direction, convenient and efficient can be mounted on be relatively large in diameter, weight
In heavier tested impeller 8, using coning sleeve and the consistent tapered configuration of mounting ring, when installation only need to gently push can will be stupid
The tested impeller 8 of weight is installed on the left mounting ring 1c or right mounting ring 1e of mandrel 1；The axial length of coning sleeve is slightly less than accordingly
Mounting ring, locking nut and impeller positioning step 6 contact cooperation with tested impeller 8 respectively, can effectively fix and be tested impeller 8.
When carrying out dynamic balance of impeller detection using the utility model, as shown in figure 3, tested impeller 8 is pacified by left coning sleeve 2
On left mounting ring 1c, the wheel hub of positioning step 6 and tested impeller 8 contacts cooperation, and will be tested by left locking nut group 4
Impeller 8 is fixed；It is spirally connected on right dead ring 1f and clump weight 7 is set, the inner screw nut of the right locking nut group 5 of 7 direct replacement of clump weight,
And it is fixed by the outboard nut of right locking nut group 5.
In conclusion this patent scheme is by mandrel 1 using Double shaft-extension and cone compared with existing dynamic balance of impeller tooling
Analysis of Nested Design structure is spent, makes the generally applicable same tooling of the impeller of Multiple Type specification, improves the versatility and operability of tooling,
It improves dynamic balancing working efficiency, save cost of labor, the balance quality of design can be reached so that impeller is effectively ensured, to be promoted more
The reliability of grade turbine vacuum pump.
Claims (4)
1. a kind of multistage turbine dynamic balance of impeller tooling, detection ring (1d) and left support (1a), right support are included on mandrel (1)
(1g), it is characterised in that the mandrel (1) uses Double shaft-extension structure, and detection ring (1d) is set to the middle part of mandrel (1), left branch
Support (1a), right support (1g) are located in the left and right ends of mandrel (1), are detected and are followed successively by between ring (1d) and left support (1a)
Left mounting ring (1c), left dead ring (1b) are detected and are followed successively by right mounting ring (1e), right fastening between ring (1d) and right support (1g)
Ring (1f), left mounting ring (1c), right mounting ring (1e) diameter successively decrease from inside to outside respectively tapered structure, left mounting ring
Left coning sleeve (2), right coning sleeve (3), left dead ring (1b), right dead ring is arranged in socket respectively in (1c), right mounting ring (1e)
Helicitic texture is respectively adopted in the outer surface of (1f).
2. a kind of multistage turbine dynamic balance of impeller tooling as described in claim 1, it is characterised in that the left coning sleeve
(2), the open loop structure of circumferencial direction setting notch is respectively adopted in right coning sleeve (3).
3. a kind of multistage turbine dynamic balance of impeller tooling as described in claim 1, it is characterised in that the left coning sleeve (2),
The hole taper of right coning sleeve (3) is consistent with corresponding left mounting ring (1c), the taper of right mounting ring (1e), left coning sleeve (2), the right side
The axial length of coning sleeve (3) is less than the length of corresponding left mounting ring (1c), right mounting ring (1e), detects ring (1d) both sides of the face
Constitute the positioning step (6) of tested impeller (8).
4. a kind of multistage turbine dynamic balance of impeller tooling as described in claim 1, it is characterised in that the left dead ring
Left locking nut group (4), the right locking nut group (5) of setting and its threaded are separately connected on (1b), right dead ring (1f).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821541685.0U CN208805317U (en) | 2018-09-20 | 2018-09-20 | A kind of multistage turbine dynamic balance of impeller tooling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821541685.0U CN208805317U (en) | 2018-09-20 | 2018-09-20 | A kind of multistage turbine dynamic balance of impeller tooling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208805317U true CN208805317U (en) | 2019-04-30 |
Family
ID=66238316
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821541685.0U Expired - Fee Related CN208805317U (en) | 2018-09-20 | 2018-09-20 | A kind of multistage turbine dynamic balance of impeller tooling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208805317U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110230608A (en) * | 2019-07-29 | 2019-09-13 | 重庆江增船舶重工有限公司 | A kind of band end tooth dynamic balancing mandrel and impeller installing |
-
2018
- 2018-09-20 CN CN201821541685.0U patent/CN208805317U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110230608A (en) * | 2019-07-29 | 2019-09-13 | 重庆江增船舶重工有限公司 | A kind of band end tooth dynamic balancing mandrel and impeller installing |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107240981B (en) | Detachable magnetic suspension energy storage flywheel rotor | |
| CN208805317U (en) | A kind of multistage turbine dynamic balance of impeller tooling | |
| CN201632652U (en) | Main electric shaft installing and fixing structure based on elastic deformation of conical surface | |
| CN203818037U (en) | Magnetic assembling tool structure for round work-pieces | |
| CN104455003B (en) | Weight-reduction pin type roller bearing retainer | |
| CN201824239U (en) | Deep hole grinding motorized spindle | |
| CN104505787A (en) | Tubular bus split conductor clamp fitting | |
| CN214643166U (en) | Big gear wheel assembling and positioning device | |
| CN205805985U (en) | The General balance mandrel of fast changeable | |
| CN113154157A (en) | Quick assembling and disassembling device for end face flange | |
| CN108678813B (en) | Pull rod rotor with self-locking nut device | |
| CN202834416U (en) | Spring hanger | |
| CN220749033U (en) | Mechanical sealing device | |
| CN105650130A (en) | Installation structure for bearing outer ring and bearing seat | |
| CN202547928U (en) | Radial connection structure for test bearing and drive shaft | |
| CN220687409U (en) | Turbocharger rotor noise reduction mechanism | |
| CN211778562U (en) | Shaft sleeve for supercharger | |
| CN211701772U (en) | Motor stator press fitting mould | |
| CN109162957B (en) | Water pump | |
| CN106763195B (en) | A kind of elasticity tilting bush sliding bearing | |
| CN204985324U (en) | Flange bearing fast -assembling structure | |
| CN202031993U (en) | Novel plug of slewing bearing | |
| CN220581244U (en) | Pin positioning device for axial plunger pump | |
| CN203641276U (en) | Air bearing of tubular strander | |
| CN203906545U (en) | Slewing bearing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20190430 |