CN208651507U - A kind of effective device for solving acutely to shake when vibration fuselage is shut down - Google Patents
A kind of effective device for solving acutely to shake when vibration fuselage is shut down Download PDFInfo
- Publication number
- CN208651507U CN208651507U CN201821149605.7U CN201821149605U CN208651507U CN 208651507 U CN208651507 U CN 208651507U CN 201821149605 U CN201821149605 U CN 201821149605U CN 208651507 U CN208651507 U CN 208651507U
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- CN
- China
- Prior art keywords
- cylinder
- transverse slat
- bobbing machine
- damping spring
- sliding panel
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Abstract
A kind of effective device for solving acutely to shake when vibration fuselage is shut down.Multiple support rods are provided with above the pedestal that it includes, transverse slat is slidably connected on support rod, the first damping spring is provided with above transverse slat, it is connect above first damping spring with bobbing machine installing frame lower end surface, first cylinder is set on the base, the output end of first cylinder is connect by the first connecting plate with transverse slat, multiple columns are provided on the pedestal of transverse slat two sides, mounting plate is provided on column, mounting base is provided on mounting plate, sliding panel, sliding panel is slidably arranged on the mounting plate of bobbing machine installing frame side, sliding panel is connect with bobbing machine installing frame by the second damping spring, second cylinder is arranged in mounting base, the output end of second cylinder is connect by the second connecting plate with sliding panel.It can carry out effective buffer shock-absorbing when bobbing machine fuselage is shut down, violent shaking when preventing bobbing machine fuselage from shutting down, and can quickly stop shaking, and prolong its service life.
Description
Technical field
The utility model relates to vibration absorber technical fields, and in particular to violent when a kind of effectively solution vibration fuselage shutdown
The device of shaking.
Background technique
The vibration reducing measure of bobbing machine is mainly pasted by being mounted on the mandril shock of motor two sides in shake table reverse side at present
Yielding rubber pad realize, in work process, often occur pasting fall off in the yielding rubber pad of the reverse side of vibration table it is existing
As, and during bobbing machine is shut down, fuselage can generate violent shaking, and jitter time extends, when causing table top longer
Between cannot balance so that larger shake occurs in equipment, influence vibrating effect.
Utility model content
The purpose of this utility model is that it is in view of the drawbacks of the prior art and insufficient, a kind of effectively solution vibration fuselage is provided
The device acutely shaken when shutdown, during it can solve current bobbing machine shutdown, fuselage can generate violent shaking, shake
Time extends, and causes the table top long period that cannot balance, so that larger shake occurs in equipment, influences the defect of vibrating effect.
To achieve the above object, the utility model is using following technical scheme: it includes pedestal 1, support rod 2, transverse slat
3, the first damping spring 4, bobbing machine installing frame 5, the first cylinder 6, the first connecting plate 7, column 8, mounting plate 9, mounting base 10, cunning
Movable plate 11, the second damping spring 12, the second cylinder 13, the second connecting plate 14, the top of the pedestal 1 are provided with multiple support rods
2, transverse slat 3 is slidably connected on the support rod 2, and the top of the transverse slat 3 is provided with the first damping spring 4, and described first subtracts
Shake spring 4 top is connect with 5 lower end surface of bobbing machine installing frame, the setting of the first cylinder 6 on pedestal 1, the first cylinder 6 it is defeated
Outlet is connect by the first connecting plate 7 with transverse slat 3, is provided with multiple columns 8, the column on the pedestal 1 of 3 two sides of transverse slat
It is provided with mounting plate 9 on 8, mounting base 10, sliding panel 11 are provided on the mounting plate 9, the sliding panel 11 is slidably arranged in
On the mounting plate 9 of 5 side of bobbing machine installing frame, sliding panel 11 and bobbing machine installing frame 5 are connected by the second damping spring 12
It connects, second cylinder 13 is arranged in mounting base 10, and the output end of the second cylinder 13 passes through the second connecting plate 14 and sliding panel
11 connections.
It is provided with slide opening 2-1 on the support rod 2, slide-bar 3-1, the support rod 2 and transverse slat are provided on the transverse slat 3
3 are matched with slide-bar 3-1 by slide opening 2-1 and are slidably connected.It is slidably connected by slide-bar 3-1 and slide opening 2-1 cooperation so that first
When cylinder 6 is run, transverse slat 3 can be shifted up, to make the compression of the first damping spring 4 can be under bobbing machine installing frame 5
The vibration of end face carries out effective vibration damping.
The bottom of the sliding panel 11 is provided with sliding block 11-1, and sliding rail 9-1, the sliding are provided on the mounting plate 9
Plate 11 is slidably connected by sliding block 11-1 with matching for sliding rail 9-1 with mounting plate 9.Cooperated by sliding block 11-1 and sliding rail 9-1
When being slidably connected so that the second cylinder 13 is run, sliding panel 11 can be displaced to 5 direction of bobbing machine installing frame, to make second
The compression of damping spring 12 can carry out effective vibration damping to the vibration of 5 two sides of bobbing machine installing frame.
It also includes rubber base plate 15, and the rubber base plate 15 is arranged between pedestal 1 and the first cylinder 6.Pass through rubber
The first cylinder 6 can be effectively protected in pedestal 15, prolong its service life.
First damping spring, 4 quantity be it is multiple, multiple first damping springs 4 are uniformly arranged on transverse slat 3 and bobbing machine
Between the lower end surface of installing frame 5.Bobbing machine can be made to play the work of vibration reduction and cushioning at runtime by multiple first damping springs 4
With, and shut down by the first cylinder 6 in bobbing machine and push the first damping spring 4 of compression, bobbing machine fuselage can be prevented violent
It shakes, and quick vibration damping.
It also includes fixing seat 16, and the fixing seat 16 is arranged on the lower end surface of pedestal 1.It can be incited somebody to action by fixing seat 16
Device is stable and firm to be placed on the ground.
After adopting the above technical scheme, the utility model has the beneficial effect that its structure is simple, design rationally, can shake
Motivation fuselage carries out effective buffer shock-absorbing when shutting down, violent shaking when preventing bobbing machine fuselage from shutting down, and can be fast
The stopping of speed is shaken, and is prolonged its service life.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the enlarged drawing of part A in Fig. 1；
Fig. 3 is the enlarged drawing of part B in Fig. 1.
Description of symbols: pedestal 1, support rod 2, transverse slat 3, the first damping spring 4, bobbing machine installing frame 5, the first cylinder
6, the first connecting plate 7, column 8, mounting plate 9, mounting base 10, sliding panel 11, the second damping spring 12, the second cylinder 13, second
Connecting plate 14, rubber base plate 15, fixing seat 16, slide opening 2-1, slide-bar 3-1, sliding rail 9-1, sliding block 11-1.
Specific embodiment
Referring to shown in Fig. 1-Fig. 3, present embodiment the technical solution adopted is that: it includes pedestal 1, support rod 2, horizontal
Plate 3, the first damping spring 4, bobbing machine installing frame 5, the first cylinder 6, the first connecting plate 7, column 8, mounting plate 9, mounting base 10,
Sliding panel 11, the second damping spring 12, the second cylinder 13, the second connecting plate 14, the top of the pedestal 1 are provided with multiple supports
Bar 2, slidably connects transverse slat 3 on the support rod 2, and the top of the transverse slat 3 is provided with the first damping spring 4, and described first
4 top of damping spring is connect with 5 lower end surface of bobbing machine installing frame, and first cylinder 6 is arranged on pedestal 1, the first cylinder 6
Output end is connect by the first connecting plate 7 with transverse slat 3, and multiple columns 8 are provided on the pedestal 1 of 3 two sides of transverse slat, described vertical
It is provided with mounting plate 9 on column 8, mounting base 10, sliding panel 11, the sliding of sliding panel 11 setting are provided on the mounting plate 9
On the mounting plate 9 close to 5 side of bobbing machine installing frame, sliding panel 11 and bobbing machine installing frame 5 pass through the second damping spring 12
Connection, second cylinder 13 are arranged in mounting base 10, and the output end of the second cylinder 13 passes through the second connecting plate 14 and sliding
Plate 11 connects.
It is provided with slide opening 2-1 on the support rod 2, slide-bar 3-1, the support rod 2 and transverse slat are provided on the transverse slat 3
3 are matched with slide-bar 3-1 by slide opening 2-1 and are slidably connected.It is slidably connected by slide-bar 3-1 and slide opening 2-1 cooperation so that first
When cylinder 6 is run, transverse slat 3 can be shifted up, to make the compression of the first damping spring 4 can be under bobbing machine installing frame 5
The vibration of end face carries out effective vibration damping.
The bottom of the sliding panel 11 is provided with sliding block 11-1, and sliding rail 9-1, the sliding are provided on the mounting plate 9
Plate 11 is slidably connected by sliding block 11-1 with matching for sliding rail 9-1 with mounting plate 9.Cooperated by sliding block 11-1 and sliding rail 9-1
When being slidably connected so that the second cylinder 13 is run, sliding panel 11 can be displaced to 5 direction of bobbing machine installing frame, to make second
The compression of damping spring 12 can carry out effective vibration damping to the vibration of 5 two sides of bobbing machine installing frame.
It also includes rubber base plate 15, and the rubber base plate 15 is arranged between pedestal 1 and the first cylinder 6.Pass through rubber
The first cylinder 6 can be effectively protected in pedestal 15, prolong its service life.
First damping spring, 4 quantity be it is multiple, multiple first damping springs 4 are uniformly arranged on transverse slat 3 and bobbing machine
Between the lower end surface of installing frame 5.Bobbing machine can be made to play the work of vibration reduction and cushioning at runtime by multiple first damping springs 4
With, and shut down by the first cylinder 6 in bobbing machine and push the first damping spring 4 of compression, bobbing machine fuselage can be prevented violent
It shakes, and quick vibration damping.
It also includes fixing seat 16, and the fixing seat 16 is arranged on the lower end surface of pedestal 1.It can be incited somebody to action by fixing seat 16
Device is stable and firm to be placed on the ground.
Working principle of the utility model is: in use, pushing transverse slat to shift up by the first cylinder, to drive first
Damping spring compression squeezes the lower end surface of bobbing machine installing frame, while the second cylinder of bobbing machine installing frame two sides pushes
Sliding panel is displaced to bobbing machine installing frame side, to drive the compression of the second damping spring to two sides of bobbing machine installing frame
Squeezed, by the first damping spring, the second damping spring compression can the shaking quickly to bobbing machine fuselage delay
Punching and vibration damping shorten the time of bobbing machine fuselage shaking, to prolong its service life.
The above is merely intended for describing the technical solutions of the present application, but not for limiting the present application, those of ordinary skill in the art couple
The other modifications or equivalent replacement that the technical solution of the utility model is made, without departing from technical solutions of the utility model
Spirit and scope should all cover in the scope of the claims of the utility model.
Claims (6)
1. a kind of device for effectively solving acutely to shake when vibration fuselage is shut down, it is characterised in that: it includes pedestal (1), support
Bar (2), transverse slat (3), the first damping spring (4), bobbing machine installing frame (5), the first cylinder (6), the first connecting plate (7), column
(8), mounting plate (9), mounting base (10), sliding panel (11), the second damping spring (12), the second cylinder (13), the second connecting plate
(14), it is provided with multiple support rods (2) above the pedestal (1), slidably connects transverse slat (3), institute on the support rod (2)
It states and is provided with above transverse slat (3) the first damping spring (4), the first damping spring (4) top and bobbing machine installing frame (5)
Lower end surface connection, first cylinder (6) are arranged on pedestal (1), and the output end of the first cylinder (6) passes through the first connecting plate
(7) it is connect with transverse slat (3), is provided with multiple columns (8) on the pedestal (1) of transverse slat (3) two sides, is set on the column (8)
It is equipped with mounting plate (9), mounting base (10), sliding panel (11) is provided on the mounting plate (9), sliding panel (11) sliding is set
It sets on the mounting plate (9) close to bobbing machine installing frame (5) side, sliding panel (11) and bobbing machine installing frame (5) pass through second
Damping spring (12) connection, second cylinder (13) are arranged on mounting base (10), and the output end of the second cylinder (13) passes through
Second connecting plate (14) is connect with sliding panel (11).
2. a kind of device for effectively solving acutely to shake when vibration fuselage is shut down according to claim 1, it is characterised in that:
It is provided with slide opening (2-1) on the support rod (2), is provided with slide-bar (3-1) on the transverse slat (3), the support rod (2) and cross
Plate (3) is matched with slide-bar (3-1) by slide opening (2-1) and is slidably connected.
3. a kind of device for effectively solving acutely to shake when vibration fuselage is shut down according to claim 1, it is characterised in that:
The bottom of the sliding panel (11) is provided with sliding block (11-1), is provided with sliding rail (9-1), the sliding on the mounting plate (9)
Plate (11) is slidably connected by sliding block (11-1) with matching for sliding rail (9-1) with mounting plate (9).
4. a kind of device for effectively solving acutely to shake when vibration fuselage is shut down according to claim 1, it is characterised in that:
It also includes rubber base plate (15), and the rubber base plate (15) is arranged between pedestal (1) and the first cylinder (6).
5. a kind of device for effectively solving acutely to shake when vibration fuselage is shut down according to claim 1, it is characterised in that:
First damping spring (4) quantity be it is multiple, multiple first damping springs (4) are uniformly arranged on transverse slat (3) and bobbing machine and pacify
It frames up between the lower end surface of (5).
6. a kind of device for effectively solving acutely to shake when vibration fuselage is shut down according to claim 1, it is characterised in that:
It also includes fixing seat (16), and the fixing seat (16) is arranged on the lower end surface of pedestal (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821149605.7U CN208651507U (en) | 2018-07-18 | 2018-07-18 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821149605.7U CN208651507U (en) | 2018-07-18 | 2018-07-18 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208651507U true CN208651507U (en) | 2019-03-26 |
Family
ID=65785079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821149605.7U Expired - Fee Related CN208651507U (en) | 2018-07-18 | 2018-07-18 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208651507U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109114160A (en) * | 2018-07-12 | 2019-01-01 | 太仓怡泰霖智能科技有限公司 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
-
2018
- 2018-07-18 CN CN201821149605.7U patent/CN208651507U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109114160A (en) * | 2018-07-12 | 2019-01-01 | 太仓怡泰霖智能科技有限公司 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
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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: 20190326 Termination date: 20210718 |