CN206141899U - Automatic bundle strapping machine - Google Patents
Automatic bundle strapping machine Download PDFInfo
- Publication number
- CN206141899U CN206141899U CN201621004922.0U CN201621004922U CN206141899U CN 206141899 U CN206141899 U CN 206141899U CN 201621004922 U CN201621004922 U CN 201621004922U CN 206141899 U CN206141899 U CN 206141899U
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- CN
- China
- Prior art keywords
- fuselage
- motor
- steel wire
- roller
- strapping machine
- 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.)
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Abstract
The utility model provides an automatic bundle strapping machine, includes the fuselage, its top is equipped with material roller, pay -off motor, ties up the motor, the fuselage is the loop configuration, the bottom middle part of fuselage is equipped with material clamping component, material clamping component pass through the steel wire with it connects to tie up the motor, steel wire spiral is on the steel wire roller the winding has the ribbon on the material roller, the inboard of fuselage is equipped with the static metal sheet. The beneficial effects are that: not wasting under the condition of ribbon, guarantee to tie up the quality, simplify the structure, outside shape is regular, the the energy can be saved during material loading.
Description
Technical field
This utility model is related to Rhizoma Dioscoreae esculentae food production mechanical field, it is particularly a kind of for bean sheet jelly, bean noodles produce from
Dynamic strapper.
Background technology
The principle of tying up of existing automatic flexible strapping machine is divided into two kinds, and one kind is band to be received by tying up drive component
Tightly, another kind is turned round by feeding motor, tightens up band.The former advantage is to tie up fastening, but can waste a part of bundle
Band, when the material diameter especially tied up is less, can waste substantial amounts of band, and the latter's can be a little complete recovered material,
But as feeding motor have passed through material roller transmission, and slippage between band and material roller, is easily produced, so feeding motor is again
Zero load can be produced, effect is tied up poor.
The feeding principle of existing automatic flexible strapping machine is also classified into two kinds, and a kind of is the feeding group by being surrounded on fuselage interior
Part, the internal ring for hauling band around fuselage rotate a circle, and complete feeding, and another kind is the rear side installation loading assemblies in fuselage, front
Person needs to be equipped with the loading assemblies rotated around fuselage, and the motor being driven to loading assemblies, motor and attached
The speed change gear of category also can be rotated around fuselage with loading assemblies together, have a strong impact on the firm of fuselage, because the one of fuselage
Side need to be to be separated, if loading assemblies are carried out with steel wire traction, needs the loading assemblies of two feeding motors, the latter to be located at machine
The rear side of body, and need to complete feeding by cylinder control is movable, the length of material is limited, because the rear side of fuselage
There are loading assemblies, material has no idea to go deep into fuselage interior, and above two feeding principle, and feeding process is required to mechanical drive
Move, complex structure, and its profile is irregular.
The content of the invention
The purpose of this utility model is, in order to solve the above problems, to devise a kind of automatic flexible strapping machine.Specific design scheme
For：
A kind of automatic flexible strapping machine, including fuselage, its top are provided with material roller, feeding motor, tie up motor, and the fuselage is in ring
Shape structure, the center bottom of the fuselage are provided with material folding component, and the material folding component ties up motor connection with described by steel wire,
The steel wire winding is wound with band on the material roller on steel wire roller, and electrostatic metal plate is provided with the inside of the fuselage.
The feeding motor is located at the left side for tying up motor, the curved structure of the electrostatic metal plate, the electrostatic
Metallic plate is attached in the left side of the fuselage circulus on semi-ring, and the steel wire is through the fuselage interior, the steel
Silk is located in the right side of the fuselage circulus on semi-ring.
Band wound clockwise on the material roller is rounded on the material roller, cuts on the right side of the band circular configuration
Line is located at the surface of the fuselage material folding component, and the material folding component is the electromagnetism relay folder of two relay block compositions, described
Diameter of the distance between the two relay blocks of material folding component more than the band circular configuration.
The feeding motor, tie up motor and be bilateral servo motor, the electrostatic metal plate, feeding motor and the material
Between roller, described tying up be bonded between motor and the steel wire roller, the steel wire wrapped anti-clockwise is in the steel wire roller
On.
Photosensitive sensor is provided with the top of the internal ring of the fuselage, control assembly is installed inside the left semi-ring of the fuselage,
The photosensitive sensor, feeding motor, tie up motor, material folding component and electrically connect with the control assembly, the top of the fuselage
End is provided with cutting assembly, and the cutting assembly is the shears with heating function.
The rear and front end of two relay blocks is mounted on butterfly spring piece, the curved structure of the butterfly spring piece,
The two ends inner arc of the butterfly spring piece is fixedly connected with the relay block, and the butterfly spring piece is stage clip spring leaf.
Slideway is provided with the fuselage, the material folding component is connected with the sliding machine body by slideway, the material folding group
The curved structure of part vertical cross-section in left-right direction, is provided with multigroup tooth engaged, the occlusion in the middle part of two relay blocks
Tooth is rectangle tooth engaged, the one kind in taper tooth engaged.
The automatic flexible strapping machine obtained by above-mentioned technical proposal of the present utility model, its advantage is：
In the case where band is not wasted, it is ensured that bundling quality, simplify structure, external shape is regular, and energy is saved during feeding
Source.
Description of the drawings
Fig. 1 is automatic flexible strapping machine described in the utility model；
In figure, 1, fuselage；2nd, expect roller；3rd, feeding motor；4th, tie up motor；5th, material folding component；6th, steel wire；7th, steel wire roller；
8th, band；9th, electrostatic metal plate；10th, butterfly spring piece；11st, slideway；12nd, tooth engaged；13rd, photosensitive sensor；14th, control group
Part；15th, cutting assembly.
Specific embodiment
Below in conjunction with the accompanying drawings this utility model is specifically described.
Fig. 1 is automatic flexible strapping machine described in the utility model, as shown in figure 1, a kind of automatic flexible strapping machine, including fuselage 1, its top
End is provided with material roller 2, feeding motor 3, ties up motor 4, and the structure in a ring of the fuselage 1, the center bottom of the fuselage 1 are provided with folder
Material component 5, the material folding component 5 are connected with the motor 4 of tying up by steel wire 6, and the steel wire 6 is wound in institute on steel wire roller 7
Stating and band 8 is wound with material roller 2, the inner side of the fuselage 1 is provided with electrostatic metal plate 9.
The feeding motor 3 is located at the left side for tying up motor 4, and 9 curved structure of the electrostatic metal plate is described quiet
Electric metal plate 9 is attached in the left side of 1 circulus of the fuselage on semi-ring, the steel wire 6 through inside the fuselage 1,
The steel wire 6 is located in the right side of 1 circulus of the fuselage on semi-ring.
8 wound clockwise of band on the material roller 2 is rounded on the material roller 2, the right side of 8 circular configuration of the band
Lateral incision line is located at the surface of 1 material folding component 5 of the fuselage, and the material folding component 5 is the electromagnetism relay of two relay block compositions
The diameter of the distance between folder, two relay blocks of the material folding component 5 more than 8 circular configuration of the band.
The feeding motor 3, tie up motor 4 and be bilateral servo motor, the electrostatic metal plate 9, feeding motor 3 and institute
State between material roller 2, described tying up is bonded between motor 4 and the steel wire roller 7,6 wrapped anti-clockwise of the steel wire is in institute
State on steel wire roller 7.
Photosensitive sensor 13 is provided with the top of the internal ring of the fuselage 1, control group is installed inside the left semi-ring of the fuselage 1
Part 14, the photosensitive sensor 13, feeding motor 3, is tied up motor 4, material folding component 5 and is electrically connected with the control assembly 14,
The top of the fuselage 1 is provided with cutting assembly 15, and the cutting assembly 15 is the shears with heating function.
The rear and front end of two relay blocks is mounted on butterfly spring piece 10,10 curved knot of the butterfly spring piece
Structure, the two ends inner arc of the butterfly spring piece 10 are fixedly connected with the relay block, and the butterfly spring piece 10 is stage clip spring
Piece.
Slideway 11 is provided with the fuselage 1, the material folding component 5 is slidably connected with the fuselage 1 by slideway 11, described
The curved structure of the vertical cross-section in left-right direction of material folding component 5, is provided with multigroup tooth engaged 12 in the middle part of two relay blocks,
The tooth engaged 12 is rectangle tooth engaged, the one kind in taper tooth engaged.
Feeding step：
Feeding motor 3 is started, rotates clockwise the material roller 2, the band 8 on roller 2 is expected to dropping material, the band 8
End under when falling between two relay blocks, complete feeding.
Feeding process, it is only necessary to provide a small amount of power, simple structure, save energy to feeding motor 3.
Tie up step：
After feeding, the internal ring of fuselage 1 is divided into two semicircles by the band 8, is put into material from the semicircle positioned at right side,
The photosensitive sensor 13 receives the signal that material is put into,
The material folding component 5 is closed, and the end of band 8 is clipped between tooth engaged 12,
The electrostatic metal plate 9 starts, and band 8 is adsorbed and fits with the electrostatic metal plate 9,
The motor 4 of tying up starts, and makes material folding component that the top of fuselage 1 is moved to along slideway 11 by the traction of steel wire 6,
3 rotate counterclockwise of the feeding motor, band 8 is tightened on material roller 2,
Again by motor 4 is tied up, band 8 of tying tight,
Band 8 in " u " shape structure is engaged in a ring by the cutting assembly 15, by making bundle to the heating of cutting assembly 15
Band 8 fuses, and is bonded together.
In said process, if material diameter is less, band 8 can not be adsorbed by electrostatic metal plate 9, if material
It is relatively large in diameter, can be arranged by control assembly 14, realize following feeding steps：
Feeding motor 3 is started, rotates clockwise the material roller 2,
Band 8 on material roller 2 is fallen under the end of the band 8 between two relay blocks to dropping material,
The material folding component 5 is closed, and the end of band 8 is clipped between tooth engaged 12,
The electrostatic metal plate 9 starts, and band 8 is adsorbed and fits with the electrostatic metal plate 9.
After the band 8 is adsorbed with electrostatic metal plate 9, continued power is needed to ensure adsorbed state.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solutions of the utility model, the technology of the art
Some variations that personnel may be made to some of which part embody principle of the present utility model, belong to this utility model
Protection domain within.
Claims (7)
1. a kind of automatic flexible strapping machine, including fuselage (1), its top are provided with material roller (2), feeding motor (3), tie up motor (4), its
It is characterised by, the fuselage (1) structure in a ring, the center bottom of the fuselage (1) are provided with material folding component (5), the material folding
Component (5) is connected with the motor (4) of tying up by steel wire (6), and the steel wire (6) is wound in the material roller on steel wire roller (7)
(2) band (8) is wound with, on the inside of the fuselage (1), electrostatic metal plate (9) is provided with.
2. according to the automatic flexible strapping machine described in claim 1, it is characterised in that the feeding motor (3) is tied up positioned at described
The left side of motor (4), the curved structure of the electrostatic metal plate (9), the electrostatic metal plate (9) are attached to the fuselage (1)
In the left side of circulus on semi-ring, the steel wire (6) is internal through the fuselage (1), and the steel wire (6) is positioned at the machine
In the right side of body (1) circulus on semi-ring.
3. according to the automatic flexible strapping machine described in claim 1, it is characterised in that the band (8) on the material roller (2) is clockwise
It is wound in rounded on the material roller (2), the right side tangent line of band (8) circular configuration is located at the fuselage (1) material folding group
The surface of part (5), the material folding component (5) they are that the electromagnetism relay of two relay block compositions is pressed from both sides, the two of the material folding component (5)
Diameter of the distance between the individual relay block more than the band (8) circular configuration.
4. according to the automatic flexible strapping machine described in claim 1, it is characterised in that the feeding motor (3), tie up motor (4)
Bilateral servo motor is, between the electrostatic metal plate (9), feeding motor (3) and the material roller (2), described motor is tied up
(4) it is bonded between the steel wire roller (7), steel wire (6) wrapped anti-clockwise is on the steel wire roller (7).
5. according to the automatic flexible strapping machine described in claim 1, it is characterised in that be provided with sense at the top of the internal ring of the fuselage (1)
Optical sensor (13), is provided with control assembly (14) inside the left semi-ring of the fuselage (1), the photosensitive sensor (13), send
Material motor (3), tie up motor (4), material folding component (5) and electrically connect with the control assembly (14), the top of the fuselage (1)
Cutting assembly (15) is provided with, the cutting assembly (15) is the shears with heating function.
6. according to the automatic flexible strapping machine described in claim 3, it is characterised in that pacify the rear and front end of two relay blocks
Equipped with butterfly spring piece (10), the curved structure of the butterfly spring piece (10), the two ends inner arc of the butterfly spring piece (10)
It is fixedly connected with the relay block, the butterfly spring piece (10) is stage clip spring leaf.
7. according to the automatic flexible strapping machine described in claim 3, it is characterised in that be provided with slideway (11), institute in the fuselage (1)
State material folding component (5) to be slidably connected with the fuselage (1) by slideway (11), the material folding component (5) in left-right direction hang down
The curved structure in straightforward face, is provided with multigroup tooth engaged (12) in the middle part of two relay blocks, the tooth engaged (12) is rectangle
One kind in tooth engaged, taper tooth engaged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621004922.0U CN206141899U (en) | 2016-08-30 | 2016-08-30 | Automatic bundle strapping machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621004922.0U CN206141899U (en) | 2016-08-30 | 2016-08-30 | Automatic bundle strapping machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206141899U true CN206141899U (en) | 2017-05-03 |
Family
ID=58617875
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621004922.0U Expired - Fee Related CN206141899U (en) | 2016-08-30 | 2016-08-30 | Automatic bundle strapping machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206141899U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111684989A (en) * | 2020-07-22 | 2020-09-22 | 姜蕾蕾 | Edible mushroom bag opening closing device |
| CN116534333A (en) * | 2023-07-05 | 2023-08-04 | 黑龙江省农业科学院绥化分院 | Industrial hemp bundling equipment |
-
2016
- 2016-08-30 CN CN201621004922.0U patent/CN206141899U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111684989A (en) * | 2020-07-22 | 2020-09-22 | 姜蕾蕾 | Edible mushroom bag opening closing device |
| CN116534333A (en) * | 2023-07-05 | 2023-08-04 | 黑龙江省农业科学院绥化分院 | Industrial hemp bundling equipment |
| CN116534333B (en) * | 2023-07-05 | 2023-09-19 | 黑龙江省农业科学院绥化分院 | Industrial hemp bundling equipment |
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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 |
Granted publication date: 20170503 Termination date: 20170830 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |