CN109114160A - 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
- CN109114160A CN109114160A CN201810766231.1A CN201810766231A CN109114160A CN 109114160 A CN109114160 A CN 109114160A CN 201810766231 A CN201810766231 A CN 201810766231A CN 109114160 A CN109114160 A CN 109114160A
- Authority
- CN
- China
- Prior art keywords
- cylinder
- transverse slat
- bobbing machine
- damping spring
- sliding panel
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M5/00—Engine beds, i.e. means for supporting engines or machines on foundations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M7/00—Details of attaching or adjusting engine beds, frames, or supporting-legs on foundation or base; Attaching non-moving engine parts, e.g. cylinder blocks
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Sewing Machines And Sewing (AREA)
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 present invention relates to vibration absorber technical fields, and in particular to a kind of effectively to solve acutely to shake when vibration fuselage is shut down
Device.
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.
Summary of the invention
In view of the defects and deficiencies of the prior art, the present invention intends to provide a kind of vibration fuselages that effectively solves to shut down
When the device that acutely shakes, it can solve during current bobbing machine shuts down, and fuselage can generate violent shaking, jitter time
Extend, cause 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 present invention is using following technical scheme: it includes pedestal 1, support rod 2, transverse slat 3, the
One 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 support rods 2, institute
It states and slidably connects transverse slat 3 on support rod 2, the top of the transverse slat 3 is provided with the first damping spring 4, the first damping bullet
4 top of spring is connect with 5 lower end surface of bobbing machine installing frame, and first cylinder 6 is arranged on pedestal 1, the output end of the first cylinder 6
It is connect by the first connecting plate 7 with transverse slat 3, is provided with multiple columns 8 on the pedestal 1 of 3 two sides of transverse slat, on the column 8
It is provided with mounting plate 9, mounting base 10, sliding panel 11 are provided on the mounting plate 9, the sliding panel 11 is slidably arranged in close
On the mounting plate 9 of 5 side of bobbing machine installing frame, sliding panel 11 is connect with bobbing machine installing frame 5 by the second damping spring 12, institute
It states the second cylinder 13 to be arranged in mounting base 10, the output end of the second cylinder 13 is connected by the second connecting plate 14 with sliding panel 11
It 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.
After adopting the above technical scheme, design rationally, can be in bobbing machine the invention has the following beneficial effects: its structure is simple
Fuselage carries out effective buffer shock-absorbing when shutting down, violent shaking when preventing bobbing machine fuselage from shutting down, and can be quick
Stop shaking, prolong its service life.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention without any creative labor, may be used also for those of ordinary skill in the art
To obtain other drawings based on these drawings.
Fig. 1 is structural schematic diagram of the invention；
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.
The working principle of the invention: in use, pushing transverse slat to shift up by the first cylinder, to drive the first damping
Spring-compressed squeezes the lower end surface of bobbing machine installing frame, while the second cylinder of bobbing machine installing frame two sides pushes sliding
Plate is displaced to bobbing machine installing frame side, so that the compression of the second damping spring be driven to carry out two sides of bobbing machine installing frame
Squeeze, by the first damping spring, the second damping spring compression can quickly the shaking to bobbing machine fuselage carry out buffering and
Vibration damping shortens the time of bobbing machine fuselage shaking, to prolong its service life.
The above is only used to illustrate the technical scheme of the present invention and not to limit it, and those of ordinary skill in the art are to this hair
The other modifications or equivalent replacement that bright technical solution is made, as long as it does not depart from the spirit and scope of the technical scheme of the present invention,
It is intended to be within the scope of the claims of the invention.
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 |
|---|---|---|---|
| CN201810766231.1A CN109114160A (en) | 2018-07-12 | 2018-07-12 | 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 |
|---|---|---|---|
| CN201810766231.1A CN109114160A (en) | 2018-07-12 | 2018-07-12 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109114160A true CN109114160A (en) | 2019-01-01 |
Family
ID=64862124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810766231.1A Withdrawn CN109114160A (en) | 2018-07-12 | 2018-07-12 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109114160A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110500333A (en) * | 2019-08-28 | 2019-11-26 | 扬州大山液压气动制造有限公司 | A kind of multi-cavity high thrust energy saving cylinder |
| CN110649749A (en) * | 2019-11-13 | 2020-01-03 | 芜湖德力电机有限公司 | Motor fixing and supporting device |
| CN114289140A (en) * | 2021-12-08 | 2022-04-08 | 四川金杠杆机械有限公司 | Vibration/noise reduction structure and ultrafine pulverizer thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1992021912A1 (en) * | 1991-05-31 | 1992-12-10 | Platus David L | Vibration isolation system |
| CN205089893U (en) * | 2015-10-07 | 2016-03-16 | 陕西理工学院 | Damping device for mechanical equipment |
| CN105864354A (en) * | 2016-06-03 | 2016-08-17 | 湖州吉昌丝绸有限公司 | Damping device for printing and dyeing cloth dehydrator |
| CN205639443U (en) * | 2016-05-16 | 2016-10-12 | 温州江硕车业股份有限公司 | Motorcycle bumper shock absorber adjusting device |
| CN206785917U (en) * | 2017-03-22 | 2017-12-22 | 嵊州市长乐华辉电器厂 | A kind of damping feet for motor work |
| CN208651507U (en) * | 2018-07-18 | 2019-03-26 | 河北瑞雪谷物精选机械制造有限公司 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
-
2018
- 2018-07-12 CN CN201810766231.1A patent/CN109114160A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1992021912A1 (en) * | 1991-05-31 | 1992-12-10 | Platus David L | Vibration isolation system |
| CN205089893U (en) * | 2015-10-07 | 2016-03-16 | 陕西理工学院 | Damping device for mechanical equipment |
| CN205639443U (en) * | 2016-05-16 | 2016-10-12 | 温州江硕车业股份有限公司 | Motorcycle bumper shock absorber adjusting device |
| CN105864354A (en) * | 2016-06-03 | 2016-08-17 | 湖州吉昌丝绸有限公司 | Damping device for printing and dyeing cloth dehydrator |
| CN206785917U (en) * | 2017-03-22 | 2017-12-22 | 嵊州市长乐华辉电器厂 | A kind of damping feet for motor work |
| CN208651507U (en) * | 2018-07-18 | 2019-03-26 | 河北瑞雪谷物精选机械制造有限公司 | A kind of effective device for solving acutely to shake when vibration fuselage is shut down |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110500333A (en) * | 2019-08-28 | 2019-11-26 | 扬州大山液压气动制造有限公司 | A kind of multi-cavity high thrust energy saving cylinder |
| CN110649749A (en) * | 2019-11-13 | 2020-01-03 | 芜湖德力电机有限公司 | Motor fixing and supporting device |
| CN114289140A (en) * | 2021-12-08 | 2022-04-08 | 四川金杠杆机械有限公司 | Vibration/noise reduction structure and ultrafine pulverizer thereof |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190101 |
|
| WW01 | Invention patent application withdrawn after publication |