CN204074992U - A kind of elasticity filling device - Google Patents
A kind of elasticity filling device Download PDFInfo
- Publication number
- CN204074992U CN204074992U CN201420507778.7U CN201420507778U CN204074992U CN 204074992 U CN204074992 U CN 204074992U CN 201420507778 U CN201420507778 U CN 201420507778U CN 204074992 U CN204074992 U CN 204074992U
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- China
- Prior art keywords
- punching press
- knockout rod
- fuselage
- disc spring
- knock
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- 238000004080 punching Methods 0.000 claims abstract description 54
- 239000000203 mixture Substances 0.000 claims abstract description 4
- 230000000694 effects Effects 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000011265 semifinished product Substances 0.000 description 2
- 230000001070 adhesive Effects 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reaction Methods 0.000 description 1
Abstract
The utility model discloses a kind of elasticity filling device, comprise fuselage, knockout rod, damper mechanism and elastic ejection mechanism, it is characterized in that, described fuselage is provided with punching press patrix and punching press counterdie, punching press patrix and punching press counterdie form the diel of workpiece, described knockout rod is connected by damper mechanism with punching press counterdie, described elastic ejection mechanism is by holder, disc spring group and knock-pin composition, described holder divides the both sides being located at fuselage, described disc spring group and holder are socketed, the upper end of described knock-pin is connected with disc spring group, the lower end of knock-pin is provided with the buffer head suitable with knockout rod.The utility model passes through the combined innovation of fuselage, knockout rod, damper mechanism and elastic ejection mechanism and syndeton thereof, there is provided a kind of structure simple, bearing capacity is strong, long service life, stable performance, the low elasticity filling device with being specially adapted to large-scale pressing equipment of noise.
Description
Technical field
The utility model relates to the technical field of high velocity ram machine, relates to a kind of elasticity filling device on high velocity ram machine in particular.
Background technology
On high velocity ram machine, slide block and patrix are when carrying out press work, and semi-finished product blank is often fitted on patrix.If just taken off by semi-finished product blank by artificial operation, obvious production efficiency reduces greatly, and there is potential safety hazard.At this moment just need that knock-out mechanism is installed and solve this problem.Commercially, because structure is unreasonable, there is the problem that bearing capacity is weak and service life is short in knock-out mechanism.But general knock-out mechanism of the prior art or device effectively do not solve the above problems.Such as Chinese patent Authorization Notice No. CN 201283673 Y, authorized announcement date on 08 05th, 2009, the name of innovation and creation is called a kind of knock-out mechanism, this Patent Case discloses a kind of dnockout structure on hydraulic press, pass through material-punching cylinder, slide block, plunger, knockout rod and the isostructural combined innovation of elastic reset member, achieve this hydraulic press and have the advantages that response is fast and production efficiency is high, but the elastic reset member of this Patent Case is Compress Spring, the anti-bearing capacity of Compress Spring is weak, on large pressing machine, stamping parts and punching press patrix have very large adhesive force, Compress Spring does not have the effect of dnockout, easily make knockout rod generation rigid contact, thus affect the service life of knockout rod.And for example Chinese patent Authorization Notice No. CN 103056240 B, authorized announcement date on 01 29th, 2014, the name of innovation and creation is called a kind of red stamping die filling device, this Patent Case discloses a kind of dnockout structure of red stamping die, pass through fuselage, drift, knockout rod, cross-arm, elastic component and the isostructural combined innovation of guide pillar, when achieving punched blank in knockout rod retraction drift, when the blank demoulding, knockout rod stretches out drift, when but the filling device of this Patent Case is applied on high velocity ram machine, the parts such as knockout rod cannot be arranged in slide block or punching press patrix, exist and inconvenient problem is installed.The utility model passes through the combined innovation of fuselage, knockout rod, damper mechanism and elastic ejection mechanism and syndeton thereof, there is provided a kind of structure simple, bearing capacity is strong, long service life, stable performance, the low elasticity filling device with being specially adapted to large-scale pressing equipment of noise.
Summary of the invention
The filling device that the utility model solves general pressing equipment in prior art does not effectively solve the problem that bearing capacity is weak and service life is short, a kind of elasticity filling device is provided, by the combined innovation of fuselage, knockout rod, damper mechanism and elastic ejection mechanism and syndeton thereof, realizing this elasticity filling device, to have structure simple, bearing capacity is strong, long service life, stable performance, the low feature with being specially adapted to large-scale pressing equipment of noise.
In order to solve the technical problem of above-mentioned existence, the utility model takes following technical proposals: a kind of elasticity filling device, comprise fuselage, knockout rod, damper mechanism and elastic ejection mechanism, it is characterized in that, described fuselage is provided with punching press patrix and punching press counterdie, punching press patrix and punching press counterdie form the diel of workpiece, described knockout rod is connected by damper mechanism with punching press counterdie, described elastic ejection mechanism is by holder, disc spring group and knock-pin composition, described holder divides the both sides being located at fuselage, described disc spring group and holder are socketed, the upper end of described knock-pin is connected with disc spring group, the lower end of knock-pin is provided with the buffer head suitable with knockout rod.
When high velocity ram machine carries out press work, bent axle on fuselage drives punching press patrix to move downward, the press work to workpiece is completed together with the punching press counterdie of underbelly, and can be fitted on punching press patrix at workpiece, workpiece moves upward together with punching press patrix, dnockout bridge is on the top of workpiece, also move upward with workpiece, now the knock-pin of elastic ejection device effectively stops knockout rod and workpiece to move upward, make workpiece and depart from punching press patrix, knockout rod falls back original position, takes out the workpiece that punching press completes, waits for the punching press of next workpiece.Damper mechanism, after workpiece is separated with punching press patrix by knockout rod, prevents knockout rod and punching press counterdie generation rigid collision, both noise was reduced, extend again the service life of knockout rod, effectively reduce dnockout vibration of bar simultaneously, ensure the stationary performance of high velocity ram machine work; Elastic ejection mechanism, effectively stop workpiece and knockout rod to move upward, realize knockout rod and be separated with punching press patrix by workpiece, having flexible feature is to prevent knockout rod generation deformation, extends the service life of knockout rod; Holder, is generally arranged on fuselage by bolt group; Disc spring group, structure is simple, and compared with general spring, its bearing capacity is strong, is specially adapted to large-scale pressing equipment; Have the knock-pin of buffer head, structure is simple, prevents knockout rod generation rigid collision, both reduces noise, extend again the service life of knockout rod.
As preferably, described damper mechanism is made up of shock-absorbing spring and lead, and the two ends of described shock-absorbing spring are connected with knockout rod with punching press counterdie respectively, described lead and shock-absorbing spring suitable, lead and knockout rod are socketed, and lower end and the punching press counterdie of lead fix.Shock-absorbing spring, has the feature of simple structure and good damping effect; Lead, effectively prevents knockout rod displacement in the course of the work, ensures that knockout rod continues to be separated stability and the accuracy of workpiece and punching press patrix.
As preferably, the both sides of described fuselage are respectively equipped with the cushion pad suitable with knockout rod.Cushion pad, structure is simple, reduces knockout rod generation rigid collision further, extends the service life of knockout rod.
As preferably, described elastic ejection mechanism also comprises locating dowel and limiting plate, described locating dowel and disc spring group are socketed, the two ends of locating dowel fix with holder respectively, described limiting plate and locating dowel are socketed, the upper surface of limiting plate and disc spring group close contact, lower surface and the knock-pin of limiting plate fix.By increasing locating dowel and limiting plate, realizing many group disc spring groups can be installed in a holder, to improve the bearing capacity of elastic ejection device, making this elasticity filling device be more suitable for large-scale pressing equipment.
As preferably, in each described holder, be provided with 1-4 group disc spring group.The disc spring group of certain group of number, had both met the designing requirement of bearing capacity, easy for installation again.
Owing to taking above-mentioned technical scheme, a kind of elasticity filling device that the utility model provides has such beneficial effect: by the combined innovation of fuselage, knockout rod, damper mechanism and elastic ejection mechanism and syndeton thereof, there is provided a kind of structure simple, bearing capacity is strong, long service life, stable performance, the low elasticity filling device with being specially adapted to large-scale pressing equipment of noise.
Accompanying drawing explanation
Accompanying drawing 1 is a kind of structural representation of the present utility model;
Accompanying drawing 2 is that the A of the utility model accompanying drawing 1 is to enlarged drawing;
Accompanying drawing 3 is that the B of the utility model accompanying drawing 1 is to enlarged drawing.
In figure: fuselage 1 knockout rod 2 punching press patrix 3 punching press counterdie 4 holder 5 disc spring group 6 knock-pin 7 buffer head 8 shock-absorbing spring 9 lead 10 cushion pad 11 locating dowel 12 limiting plate 13.
Detailed description of the invention
Accompanying drawings, is described in further detail of the present utility model:
Embodiment one: by reference to the accompanying drawings 1 and 3, a kind of elasticity filling device, comprise fuselage 1, knockout rod 2, damper mechanism and elastic ejection mechanism, fuselage 1 is provided with punching press patrix 3 and punching press counterdie 4, punching press patrix 3 and punching press counterdie 4 form the diel of workpiece, knockout rod 2 is connected by damper mechanism with punching press counterdie 4, elastic ejection mechanism is by holder 5, disc spring group 6 and knock-pin 7 form, holder 5 points is located at the both sides of fuselage 1, disc spring group 6 and holder 5 are socketed, the upper end of knock-pin 7 is connected with disc spring group 6, the lower end of knock-pin 7 is provided with the buffer head 8 suitable with knockout rod 2.
When high velocity ram machine carries out press work, bent axle on fuselage drives punching press patrix to move downward, the press work to workpiece is completed together with the punching press counterdie of underbelly, and can be fitted on punching press patrix at workpiece, workpiece moves upward together with punching press patrix, dnockout bridge is on the top of workpiece, also move upward with workpiece, now the knock-pin of elastic ejection device effectively stops knockout rod and workpiece to move upward, make workpiece and depart from punching press patrix, knockout rod falls back original position, takes out the workpiece that punching press completes, waits for the punching press of next workpiece.
Embodiment two: by reference to the accompanying drawings 1, 2 and 3, a kind of elasticity filling device, comprise fuselage 1, knockout rod 2, damper mechanism and elastic ejection mechanism, fuselage 1 is provided with punching press patrix 3 and punching press counterdie 4, punching press patrix 3 and punching press counterdie 4 form the diel of workpiece, knockout rod 2 is connected by damper mechanism with punching press counterdie 4, damper mechanism is made up of shock-absorbing spring 9 and lead 10, the two ends of shock-absorbing spring 9 are connected with knockout rod 2 with punching press counterdie 4 respectively, lead 10 is suitable with shock-absorbing spring 9, lead 10 and knockout rod 2 are socketed, lower end and the punching press counterdie 4 of lead 10 fix, elastic ejection mechanism is by holder 5, disc spring group 6, knock-pin 7, locating dowel 12 and limiting plate 13 form, holder 5 points is located at the both sides of fuselage 1, 2 groups of disc spring groups 6 are provided with in each holder 5, disc spring group 6 and locating dowel 12 are socketed, the two ends of locating dowel 12 fix with holder 5 respectively, limiting plate 13 and locating dowel 12 are socketed, the upper surface of limiting plate 13 and disc spring group 6 close contact, lower surface and the knock-pin 7 of limiting plate 13 fix, the lower end of knock-pin 7 is provided with the buffer head 8 suitable with knockout rod 2, the both sides of fuselage 1 are respectively equipped with the cushion pad 11 suitable with knockout rod 2.
Above-described two specific embodiments, are described in detail the utility model.Apply specific embodiment herein to set forth principle of the present utility model and embodiment, the explanation of embodiment just understands core concept of the present utility model for helping.Should be understood that; for those skilled in the art; under the prerequisite not departing from the utility model core concept; some modifications can also be carried out to the utility model; the concrete technical parameter etc. of the concrete shape feature of such as knockout rod, the length of knock-pin and disc spring and damping spring carries out the combination that some amendments or claim carry out some feasibilities, within the protection domain that should drop on the utility model claim.
Claims (5)
1. an elasticity filling device, comprise fuselage (1), knockout rod (2), damper mechanism and elastic ejection mechanism, it is characterized in that, described fuselage (1) is provided with punching press patrix (3) and punching press counterdie (4), punching press patrix (3) and punching press counterdie (4) form the diel of workpiece, described knockout rod (2) is connected by damper mechanism with punching press counterdie (4), described elastic ejection mechanism is by holder (5), disc spring group (6) and knock-pin (7) composition, described holder (5) point is located at the both sides of fuselage (1), described disc spring group (6) and holder (5) are socketed, the upper end of described knock-pin (7) is connected with disc spring group (6), the lower end of knock-pin (7) is provided with the buffer head (8) suitable with knockout rod (2).
2. a kind of elasticity filling device according to claim 1, it is characterized in that, described damper mechanism is made up of shock-absorbing spring (9) and lead (10), the two ends of described shock-absorbing spring (9) are connected with knockout rod (2) with punching press counterdie (4) respectively, described lead (10) is suitable with shock-absorbing spring (9), lead (10) and knockout rod (2) are socketed, and lower end and the punching press counterdie (4) of lead (10) fix.
3. a kind of elasticity filling device according to claim 1, is characterized in that, the both sides of described fuselage (1) are respectively equipped with the cushion pad (11) suitable with knockout rod (2).
4. a kind of elasticity filling device according to claim 1, it is characterized in that, described elastic ejection mechanism also comprises locating dowel (12) and limiting plate (13), described locating dowel (12) and disc spring group (6) are socketed, the two ends of locating dowel (12) fix with holder (5) respectively, described limiting plate (13) and locating dowel (12) are socketed, and the upper surface of limiting plate (13) and disc spring group (6) close contact, lower surface and the knock-pin (7) of limiting plate (13) fix.
5. a kind of elasticity filling device according to claim 1 or 4, is characterized in that, is provided with 1-4 group disc spring group (6) in each described holder (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420507778.7U CN204074992U (en) | 2014-09-04 | 2014-09-04 | A kind of elasticity filling device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420507778.7U CN204074992U (en) | 2014-09-04 | 2014-09-04 | A kind of elasticity filling device |
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| Publication Number | Publication Date |
|---|---|
| CN204074992U true CN204074992U (en) | 2015-01-07 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201420507778.7U Active CN204074992U (en) | 2014-09-04 | 2014-09-04 | A kind of elasticity filling device |
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| CN (1) | CN204074992U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106739066A (en) * | 2016-12-21 | 2017-05-31 | 宁波澳玛特高精冲压机床股份有限公司 | A kind of transmission device for punch press |
| CN106739064A (en) * | 2016-12-21 | 2017-05-31 | 宁波澳玛特高精冲压机床股份有限公司 | A kind of modified punch press |
-
2014
- 2014-09-04 CN CN201420507778.7U patent/CN204074992U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106739066A (en) * | 2016-12-21 | 2017-05-31 | 宁波澳玛特高精冲压机床股份有限公司 | A kind of transmission device for punch press |
| CN106739064A (en) * | 2016-12-21 | 2017-05-31 | 宁波澳玛特高精冲压机床股份有限公司 | A kind of modified punch press |
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| GR01 | Patent grant |