CN205800026U - A kind of injection machine matched moulds frame assembly - Google Patents
A kind of injection machine matched moulds frame assembly Download PDFInfo
- Publication number
- CN205800026U CN205800026U CN201620659473.7U CN201620659473U CN205800026U CN 205800026 U CN205800026 U CN 205800026U CN 201620659473 U CN201620659473 U CN 201620659473U CN 205800026 U CN205800026 U CN 205800026U
- Authority
- CN
- China
- Prior art keywords
- frame assembly
- girder
- vibration damper
- injection machine
- rotor plate
- 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
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- Road Paving Machines (AREA)
- Presses And Accessory Devices Thereof (AREA)
Abstract
The utility model discloses a kind of injection machine matched moulds frame assembly; including H type shaped steel fuselage girder; being provided with shockproof feet bottom described fuselage girder, described shockproof feet includes base, described base is horizontally arranged with rotating shaft; described rotating shaft is fixing with rotor plate to be connected; it is provided with damping spring on described rotor plate, described damping spring upper end is provided with vibration damper plate, described vibration damper plate is provided with guide post; being provided with pilot hole on described rotor plate, described guide post stretches into described pilot hole.The welding process using this structure to make frame assembly can reduce girder ensures that girder is indeformable, arranges shockproof feet simultaneously and reduce vibration bottom frame assembly.
Description
Technical field
This utility model belongs to injection machine technical field, specifically a kind of injection machine matched moulds frame assembly.
Background technology
Injection machine matched moulds matched moulds frame assembly is the base of injection machine, and former fuselage girder uses iron plate welding, fuselage intensity
Deficiency, deflection is big.Cause greatly out-of-flatness bottom frame assembly due to deflection, the ground out-of-flatness simultaneously installed causes injection
Injustice installed by machine, and fuselage shaking is big, causes the Product Precision being molded into causes certain impact.
Utility model content
This utility model is not enough for prior art, it is provided that a kind of injection machine matched moulds frame assembly, this injection machine clapper die spotting press
Body assembly can reduce the welding process of girder and ensure that girder is indeformable, arranges simultaneously and can regulate height bottom frame assembly
Shockproof feet ensure standard of fuselage install, reduce vibration.
In order to solve above-mentioned technical problem, this utility model is addressed by following technical proposals: a kind of injection machine closes
Mould frame assembly, including H type shaped steel fuselage girder, is provided with shockproof feet, described shockproof feet bag bottom described fuselage girder
Including base, described base is horizontally arranged with rotating shaft, described rotating shaft is fixing with rotor plate to be connected, and described rotor plate is provided with and subtracts
Shake spring, described damping spring upper end is provided with vibration damper plate, described vibration damper plate is provided with guide post, described rotor plate sets
Being equipped with pilot hole, described guide post stretches into described pilot hole.This structure is used to make frame assembly can reduce the weldering of girder
Termination process ensures that girder is indeformable, arranges shockproof feet simultaneously and reduce vibration bottom frame assembly.
In technique scheme, it is preferred that described vibration damper plate upper end is provided with DOCK LEVELER, described DOCK LEVELER with
It is bolted between described vibration damper plate.Frame assembly is enable to be arranged on irregular ground by this kind of structure, logical
The guarantee standard of fuselage overregulating height is installed.
This utility model compared with prior art, has the advantages that this structure of employing makes frame assembly energy
The welding process enough reducing girder ensures that girder is indeformable, arranges shockproof feet simultaneously and reduce vibration bottom frame assembly.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the sectional structure schematic diagram of shockproof feet.
Detailed description of the invention
With detailed description of the invention, this utility model is described in further detail below in conjunction with the accompanying drawings: see Fig. 1 to Fig. 2,
A kind of injection machine matched moulds frame assembly, including H type shaped steel fuselage girder 1, is provided with shockproof feet 2 bottom described fuselage girder 1,
Described shockproof feet 2 includes base 21, and described base 21 is horizontally arranged with rotating shaft 22, and described rotating shaft 22 is fixed with rotor plate 23
Connect, described rotor plate 23 is provided with damping spring 24, described damping spring 24 upper end is provided with vibration damper plate 25, described in subtract
Being provided with guide post 26 on shake plate 25, described rotor plate 23 is provided with pilot hole 27, described guide post 26 stretches into described guiding
Hole 27.The welding process using this structure to make frame assembly can reduce girder ensures that girder is indeformable, simultaneously at fuselage
Component bottom arranges shockproof feet and reduces vibration.
Described vibration damper plate 25 upper end is provided with DOCK LEVELER 28, between described DOCK LEVELER 28 and described vibration damper plate 25
Connected by bolt 29.Frame assembly is enable to be arranged on irregular ground by this kind of structure, by regulation height
Ensure that standard of fuselage is installed.
Claims (2)
1. an injection machine matched moulds frame assembly, it is characterised in that: include H type shaped steel fuselage girder (1), described fuselage girder
(1) bottom is provided with shockproof feet (2), and described shockproof feet (2) includes that base (21), described base are horizontally arranged with on (21)
Rotating shaft (22), described rotating shaft (22) is fixing with rotor plate (23) to be connected, and described rotor plate (23) is provided with damping spring (24),
It is provided with vibration damper plate (25) on described damping spring (24) upper end, described vibration damper plate (25) is provided with guide post (26), described
Being provided with pilot hole (27) on rotor plate (23), described guide post (26) stretches into described pilot hole (27).
2. a kind of injection machine matched moulds frame assembly as claimed in claim 1, it is characterised in that: described vibration damper plate (25) upper end sets
It is equipped with DOCK LEVELER (28), is connected by bolt (29) between described DOCK LEVELER (28) with described vibration damper plate (25).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620659473.7U CN205800026U (en) | 2016-06-29 | 2016-06-29 | A kind of injection machine matched moulds frame assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620659473.7U CN205800026U (en) | 2016-06-29 | 2016-06-29 | A kind of injection machine matched moulds frame assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205800026U true CN205800026U (en) | 2016-12-14 |
Family
ID=57512473
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620659473.7U Expired - Fee Related CN205800026U (en) | 2016-06-29 | 2016-06-29 | A kind of injection machine matched moulds frame assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205800026U (en) |
-
2016
- 2016-06-29 CN CN201620659473.7U patent/CN205800026U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161214 Termination date: 20180629 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |