CN203062458U - Iron wire surface processing device - Google Patents
Iron wire surface processing device Download PDFInfo
- Publication number
- CN203062458U CN203062458U CN 201220742880 CN201220742880U CN203062458U CN 203062458 U CN203062458 U CN 203062458U CN 201220742880 CN201220742880 CN 201220742880 CN 201220742880 U CN201220742880 U CN 201220742880U CN 203062458 U CN203062458 U CN 203062458U
- Authority
- CN
- China
- Prior art keywords
- main body
- fuselage main
- machine main
- pulley
- iron wire
- 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
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- Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)
Abstract
An iron wire surface processing device comprises a machine main body and an air pump, wherein a feed inlet is arranged in the middle of the top end of the machine main body, a first pulley is arranged on the top surface, beside the feed inlet, of the machine main body, a second pulley is arranged at the bottom of the inner wall of the machine main body, a feed outlet is arranged at the bottom of the side wall of the machine main body, a motor is arranged at the position of a base angle of the inner wall of the machine main body, a plurality of polishing mechanisms are arranged on two side walls of the machine main body from the feed outlet to the top surface of machine main body in an interlaced mode, each polishing mechanism comprises a gauze cylinder fixing roller and a drawing roller, all the drawing rollers are controlled by the motor, a slag discharging mouth is formed in the bottom surface of the machine main body, and the slag discharging mouth is communicated with the air pump through pipelines. The iron wire surface processing device has the advantages of being simple in structure, easy and convenient to use and capable of effectively cleaning dirt on the surfaces of iron wires and guaranteeing the roughness of the surfaces of the iron wires so as to increase the cohesiveness between coating layers and the iron wires. Meanwhile, no waste water and waste gas are discharged and environment can not be polluted.
Description
(1) technical field
The utility model relates to a kind of iron wire pre-processing device of filming, and particularly relates to a kind of iron wire surface processing equipment.
(2) background technology
At present, there has been increasing nylon bag tree lace manufacturer to bring into use the extruded type film applicator to carry out the production of nylon bag tree lace, but it is because the adhesive force requirement of clad and iron wire is very high, so must be to iron wire through handling early stage in basic process.Handling common this early stage all is to flow to corrode in electrolysis sulfuric acid, is that the iron wire surface cleaning is coarse, increases the caking property of clad and iron wire.Yet this method also will be cleaned the iron wire water after handling iron wire, causes the waste at water source, also can cause environmental pollution during sewage effluent.Can effectively clear up now iron wire surface dirt on the market and guarantee that roughness to increase clad and iron wire caking property, can not cause the iron wire of the environmental pollution pre-processing device of filming also not to be found simultaneously, remains to be developed.
(3) summary of the invention
In order to overcome the film weak point of pre-processing device of existing iron wire, the utility model provides a kind of iron wire surface processing equipment.
The technical solution of the utility model is to realize like this.
A kind of iron wire surface processing equipment of this programme, comprise fuselage main body and air pump, described fuselage main body top middle portion is provided with charging aperture, the other fuselage main body end face of this charging aperture is provided with first pulley, described fuselage main body inner wall bottom is provided with second pulley, and described first pulley and second pulley are all tangent with the perpendicular at charging aperture place; Described fuselage main body wall bottom is provided with discharging opening, and this discharging opening and the second pulley bottom tangent are in same plane; Place, described fuselage main body inner wall base angle is provided with motor; Described discharging opening is staggeredly equipped with some workpiece polishing mechanisms to the fuselage main body both sides sidewall of fuselage main body end face, described any workpiece polishing mechanism includes gauze tube stationary roll and carry-over pinch rolls; The gauze tube stationary roll of described any workpiece polishing mechanism and carry-over pinch rolls are all in the same side fuselage main body inner wall and be on the same horizontal plane; Described any stationary roll and carry-over pinch rolls bottom sides are all fixedlyed connected with the fuselage main body inner wall; Described any carry-over pinch rolls are by Electric Machine Control; Described fuselage main body bottom surface is provided with slag-drip opening, and this slag-drip opening is communicated with by pipeline with air pump.
Usefulness of the present utility model is: this device structure is simple, easy to use, the roughness that can effectively clear up iron wire surface dirt and guarantee the iron wire surface does not have the discharging of waste water and gas simultaneously to increase clad and iron wire caking property, can not pollute environment.
(4) description of drawings
Fig. 1 looks cutaway view for master of the present utility model.
Fig. 2 is vertical view cutaway drawing of the present utility model.
(5) specific embodiment
Below in conjunction with accompanying drawing the specific embodiment of the present utility model is made brief description.
A kind of iron wire surface processing equipment as figure, comprise fuselage main body 1 and air pump 2, described fuselage main body 1 top middle portion is provided with charging aperture 3, these charging aperture 3 other fuselage main body 1 end faces are provided with first pulley 4, described fuselage main body 1 inwall bottom is provided with second pulley 5, and described first pulley 4 and second pulley 5 are all tangent with charging aperture 3; Described fuselage main body 1 sidewall bottom is provided with discharging opening 6, and this discharging opening 6 and second pulley, 5 bottom tangent are in same plane; Place, described fuselage main body 1 inwall base angle is provided with motor 10; Described discharging opening 6 is staggeredly equipped with some workpiece polishing mechanisms to the fuselage main body 1 both sides sidewall of fuselage main body 1 end face, described any workpiece polishing mechanism includes gauze tube stationary roll 8 and carry-over pinch rolls 9; The gauze tube stationary roll 8 of described any workpiece polishing mechanism with carry-over pinch rolls 9 all at the same side fuselage main body 1 inwall and be on the same horizontal plane; Described any stationary roll 8 and carry-over pinch rolls 9 bottom sides are all fixedlyed connected with fuselage main body 1 inwall; Described any carry-over pinch rolls 9 are by motor 10 controls; Described fuselage main body 1 bottom surface is provided with slag-drip opening 7, and this slag-drip opening 7 and air pump 2 are communicated with by pipeline.
The course of work of this example: when using this equipment to carry out iron wire surface preparation operation, earlier iron wire is walked around from first pulley, 4 tops iron wire become and passed charging aperture 3 after vertical direction moves, thereby enter fuselage main body 1 inside, then iron wire is pulled to second pulley, 5 places of fuselage main body 1 bottom, thereby walk around from second pulley, 5 bottoms and to pass discharging opening 6 after iron wire become horizontal movement, to fix a gauze tube on each gauze tube stationary roll 8 then, with an end of the gauze on the gauze tube walk around iron wire and be connected on the carry-over pinch rolls 9 after iron wire surface closely contacts, open motor 10 and air pump 2, thereby carry-over pinch rolls 9 begin to rotate gauze is moved on the carry-over pinch rolls 9 by stationary roll 8 on the gauze tube, thereby the mobile polishing iron wire surface by gauze, iron wire surface cleaning after the polishing and roughness reach the effect of electrolysis sulfuric acid, the clad cohesive force is higher than the electrolysis sulfuric acid process, there is not the discharging of pollutant simultaneously, benefit environmental protection, it is inner and reclaim that the suction of the waste residue that polishing is dropped during iron wire by air pump 2 is discharged fuselage main body 1 from slag-drip opening 7, avoids polluting.
More than an embodiment of the present utility model is had been described in detail, but described content only is preferred embodiment of the present utility model, can not be considered to for limiting practical range of the present utility model.All equalizations of doing according to the utility model application range change and improve etc., all should still belong within the patent covering scope of the present utility model.
Claims (1)
1. iron wire surface processing equipment, comprise fuselage main body (1) and air pump (2), it is characterized in that: described fuselage main body (1) top middle portion is provided with charging aperture (3), other fuselage main body (1) end face of this charging aperture (3) is provided with first pulley (4), described fuselage main body (1) inwall bottom is provided with second pulley (5), and described first pulley (4) and second pulley (5) are all tangent with the perpendicular at charging aperture (3) place; Described fuselage main body (1) sidewall bottom is provided with discharging opening (6), and this discharging opening (6) is in same plane with second pulley (5) bottom tangent; Place, described fuselage main body (1) inwall base angle is provided with motor (10); Described discharging opening (6) is staggeredly equipped with some workpiece polishing mechanisms to fuselage main body (1) the both sides sidewall of fuselage main body (1) end face, described any workpiece polishing mechanism includes gauze tube stationary roll (8) and carry-over pinch rolls (9); The gauze tube stationary roll (8) of described any workpiece polishing mechanism and carry-over pinch rolls (9) are all at the same side fuselage main body (1) inwall and be on the same horizontal plane; Described any stationary roll (8) and carry-over pinch rolls (9) bottom sides are all fixedlyed connected with fuselage main body (1) inwall; Described any carry-over pinch rolls (9) are controlled by motor (10); Described fuselage main body (1) bottom surface is provided with slag-drip opening (7), and this slag-drip opening (7) is communicated with by pipeline with air pump (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220742880 CN203062458U (en) | 2012-12-28 | 2012-12-28 | Iron wire surface processing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220742880 CN203062458U (en) | 2012-12-28 | 2012-12-28 | Iron wire surface processing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203062458U true CN203062458U (en) | 2013-07-17 |
Family
ID=48761284
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220742880 Expired - Fee Related CN203062458U (en) | 2012-12-28 | 2012-12-28 | Iron wire surface processing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203062458U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105235173A (en) * | 2014-07-08 | 2016-01-13 | 天津市龙海特种线材有限公司 | Environment-friendly wire rod production device |
| CN109877682A (en) * | 2019-02-18 | 2019-06-14 | 陈岩 | A kind of waste steel wire recovery processing technique |
-
2012
- 2012-12-28 CN CN 201220742880 patent/CN203062458U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105235173A (en) * | 2014-07-08 | 2016-01-13 | 天津市龙海特种线材有限公司 | Environment-friendly wire rod production device |
| CN109877682A (en) * | 2019-02-18 | 2019-06-14 | 陈岩 | A kind of waste steel wire recovery processing technique |
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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: 20130717 Termination date: 20141228 |
|
| EXPY | Termination of patent right or utility model |