CN107962851A - Three chamber laminating system of multilayer and its application method - Google Patents
Three chamber laminating system of multilayer and its application method Download PDFInfo
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- CN107962851A CN107962851A CN201711187826.3A CN201711187826A CN107962851A CN 107962851 A CN107962851 A CN 107962851A CN 201711187826 A CN201711187826 A CN 201711187826A CN 107962851 A CN107962851 A CN 107962851A
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- 238000010030 laminating Methods 0.000 title claims abstract description 38
- 238000000034 method Methods 0.000 title claims abstract description 32
- 230000007246 mechanism Effects 0.000 claims abstract description 137
- 230000005540 biological transmission Effects 0.000 claims abstract description 56
- 238000001816 cooling Methods 0.000 claims abstract description 46
- 238000007711 solidification Methods 0.000 claims abstract description 34
- 230000008023 solidification Effects 0.000 claims abstract description 34
- 238000010438 heat treatment Methods 0.000 claims description 19
- 238000003475 lamination Methods 0.000 claims description 14
- 230000008569 process Effects 0.000 claims description 13
- 238000003032 molecular docking Methods 0.000 claims description 7
- 230000007704 transition Effects 0.000 claims description 7
- 238000004140 cleaning Methods 0.000 claims description 6
- 238000007789 sealing Methods 0.000 claims description 4
- 238000007599 discharging Methods 0.000 claims description 3
- 230000003028 elevating effect Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 description 9
- 230000000712 assembly Effects 0.000 description 8
- 238000000429 assembly Methods 0.000 description 8
- 239000004744 fabric Substances 0.000 description 8
- 239000011521 glass Substances 0.000 description 8
- 238000005538 encapsulation Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- VIKNJXKGJWUCNN-XGXHKTLJSA-N norethisterone Chemical compound O=C1CC[C@@H]2[C@H]3CC[C@](C)([C@](CC4)(O)C#C)[C@@H]4[C@@H]3CCC2=C1 VIKNJXKGJWUCNN-XGXHKTLJSA-N 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000012536 packaging technology Methods 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 230000033764 rhythmic process Effects 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/0046—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by constructional aspects of the apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/06—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/08—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the cooling method
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/16—Drying; Softening; Cleaning
- B32B38/162—Cleaning
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/18—Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
The present invention relates to a kind of three chamber laminating system of multilayer and its application method, the laminating system includes three cavity layer press mechanism of multilayer and input mechanism and output mechanism, each layer of three cavity layer press mechanism of multilayer is equipped with and evacuates and preliminary laminater successively, solidification equipment and cooling device, the subassembly product output terminal of input mechanism is opposite with the evacuation of three cavity layer press mechanism of multilayer and the subassembly product input terminal of preliminary laminater, the subassembly product input terminal of output mechanism is opposite with the subassembly product output terminal of the cooling device of three cavity layer press mechanism of multilayer, each layer is equipped with Transmission system, input mechanism and output mechanism, which are equipped with, can lift to each layer of three cavity layer press mechanism of multilayer and the transmission platform that is docked with the Transmission system in each layer.The present invention can be worked independently at the same time with multilayer, and every layer of evacuation and preliminary laminater, solidification equipment and cooling device, which separate, sets a chamber, can also work independently at the same time per chamber；Realize and save place, Unmanned operation and efficient purpose.
Description
Technical field
The invention belongs to encapsulation technology field, and in particular to a kind of three chamber laminating system of multilayer and its application method, can answer
Encapsulation for solar cell module, it can also be used to need the other assemblies type products of laminating packaging.
Background technology
At present, with the high speed development of photovoltaic industry, especially great attention of the various countries to new energy development, green cleaning energy
Source --- solar energy.Therefore, application of the solar cell module in people live gradually increases, and is carried for the Working Life of people
Great convenience has been supplied, while has also created benefit for enterprise.And developed rapidly with industry, (solar double-glass assemblies are solar double-glass assemblies
Battery strings among layer glass sandwich two layers of EVA, two layers of EVA) etc. particular components extensive use, manually and take up an area into
This increase, the profit of component reduce, these cause very big pressure to component manufacturer.Common lamination machine is difficult to meet
The manufacturing technique requirent of the particular components such as solar double-glass assemblies, while production capacity is relatively low, cannot meet the requirement of industry at present.
Laminating system of the prior art is simple in structure, generally uses single cavity structure, as shown in Figure 1, the laminating system bag
Input stage 1, lamination level 2 and output stage 3 are included, the system production capacity is relatively low, and is difficult to meet the special solar energy group of such as solar double-glass assemblies
The process requirements of part.
The information for being disclosed in the background of invention technology segment is merely intended to deepen the reason of the general background technology to the present invention
Solution, and be not construed as recognizing or imply known to those skilled in the art existing of the information structure in any form
Technology.
The content of the invention
Can be more it is an object of the invention to provide a kind of three chamber laminating system of multilayer and its application method, the laminating system
Layer works independently at the same time, and every layer of evacuation and preliminary laminater, solidification equipment and cooling device, which separate, sets a chamber, per chamber
It can at the same time work independently, effectively increase production efficiency；In addition the three chamber laminating system of multilayer is also equipped with forcing cooling, upper chamber to add
Heat, transition heating function, are applicable not only to the encapsulation of the general components of solar cell, while be also applied for the spies such as solar double-glass assemblies
The encapsulation of different solar components.
The purpose of the present invention is what is be achieved through the following technical solutions：
A kind of three chamber laminating system of multilayer, including three cavity layer press mechanism of multilayer and be separately positioned on close to the multilayer three
The input mechanism and output mechanism at cavity layer press mechanism both ends, each layer of the three cavity layer press mechanism of multilayer is equipped with successively to be used for
The evacuation of laminated compenent product is with preliminary laminater, the solidification equipment for curing assembly product and for cooling component product
Cooling device, the evacuation of the subassembly product output terminal of the input mechanism and the three cavity layer press mechanism of multilayer and be tentatively laminated
The subassembly product input terminal of device is opposite, the subassembly product input terminal of the output mechanism and the three cavity layer press mechanism of multilayer
The subassembly product output terminal of cooling device is opposite, and each layer of the three cavity layer press mechanism of multilayer is equipped with the evacuation
The Transmission system of transmission assembly product, the input between preliminary laminater, the solidification equipment and the cooling device
Mechanism and the output mechanism be equipped with can lift to each layer of the three cavity layer press mechanism of multilayer and with each layer
The transmission platform of the Transmission system docking.
Preferably, each layer of the three cavity layer press mechanism of multilayer is independent control.
Preferably, the evacuation in each layer of the three cavity layer press mechanism of multilayer and preliminary laminater, described solid
It is independent control that makeup, which is put with the cooling device,.
Preferably, the end of the three cavity layer press mechanism of multilayer is equipped with cleaning systems.
Preferably, each layer of the evacuation of the three cavity layer press mechanism of multilayer and preliminary laminater and the curing
Transition heating module is equipped between device.
Preferably, the input mechanism and the output mechanism are equipped with the lifting system for lifting the transmission platform
System, the transmission platform by the decelerating motor in the jacking system and elevating chain realize lifting with three chamber of multilayer
Transmission system docking in each layer of laminate mechanism.
Preferably, the evacuation and preliminary laminater include the upper operating mechanism that can be lifted and positioned at the upper work
Lower operating mechanism below mechanism, the upper operating mechanism include with heating function upper table and with the upper table
Lower surface periphery airtight connection upper offset plate, the lower operating mechanism include with heating function lower table, it is described on
The periphery of offset plate is equipped with sealing structure.
Preferably, when the upper operating mechanism declines, closed layer is formed between the upper offset plate and the lower table
Press chamber.
Preferably, upper chamber is formed between the upper table and the upper offset plate.
Preferably, the three chamber laminating system of multilayer is included in two layers of three cavity layer press mechanisms of vertical direction arrangement, institute
The each layer for stating two layers of three cavity layer press mechanisms has been sequentially arranged the evacuation and preliminary laminater, the curing in the horizontal direction
Device and the cooling device.
The present invention another technical solution be：
A kind of application method of laminating system, the laminating system are above-mentioned three chamber laminating system of multilayer, the application method
Including step in detail below：
1) input mechanism adjusts transmission platform to height is docked with assembly line, and subassembly product is entered from pipeline
Input mechanism, input mechanism adjust transmission platform to wherein one layer of position of three cavity layer press mechanism of multilayer, and with the evacuation of this layer
Docked with preliminary laminater, subassembly product is transmitted to the evacuation of this layer and preliminary laminater, the evacuation of this layer and preliminary
Laminater carries out full-automatic evacuate and the cured process of preliminary layer according to technique initialization parameter；
2) subassembly product enters the solidification equipment of this layer by Transmission system, and the solidification equipment of this layer is joined according to technique initialization
Number, completes further lamination and solidification process；
3) subassembly product by Transmission system enter this layer cooling device, according to technique initialization parameter to subassembly product into
Row forces quick cooling；
4) output mechanism in advance adjusts transmission platform to this layer of position, the transmission platform of output mechanism and the cooling of this layer
Device docks, and subassembly product is transmitted to the transmission platform of output mechanism, and finally, output mechanism is docked with assembly line, component production
Product enter assembly line and realize discharging, complete whole lamination process.
Beneficial effects of the present invention are：
The present invention can be worked independently at the same time with multilayer, every layer of evacuation and preliminary laminater, solidification equipment and cooling dress
Put to separate and respectively set a chamber, can also work independently at the same time per chamber, flexibility is substantially improved, and effectively increases production efficiency；In addition should
Three chamber laminating system of multilayer is also equipped with forcing cooling, upper chamber heating, transition heating function, is applicable not only to the normal of solar cell
The encapsulation of component is advised, while is also applied for the encapsulation of the special solar components such as solar double-glass assemblies.The present invention is truly realized saving
Work-yard, Unmanned operation and high efficiency obtain purpose, are currently most advanced, separate unit production capacity maximum laminating machine in the world.
Brief description of the drawings
Fig. 1 is the structure diagram of laminating system of the prior art；
Fig. 2 is the structure diagram of two layers of three chamber laminating systems described in the embodiment of the present invention；
Fig. 3 is the structure diagram of the evacuation and preliminary laminater described in the embodiment of the present invention.
Description of reference numerals：
1. input stage；2. it is laminated level；3. output stage；4. two layers of three cavity layer press mechanisms；5. input mechanism；6. output mechanism；
7. first evacuates and preliminary laminater；8. the first solidification equipment；9. the first cooling device；10. second evacuates and is tentatively laminated
Device；11. the second solidification equipment；12. the second cooling device；13. transmission platform；14. jacking system；15. upper table；16.
Upper offset plate；17. lower table；18. subassembly product；19. cleaning systems；20. transition heating module；21. sealing structure.
Embodiment
With reference to specific embodiment and respective drawings, the invention will be further described.
It is to be appreciated that appended attached drawing is drawn with being not drawn to, and merely to illustrating each of the basic principle of the present invention
The suitably simplified technique of painting of kind feature.The specific design feature of invention disclosed herein include for example specific size, direction,
Position and shape will be determined partly by the specific environment to be applied and used.
In appended multiple attached drawings, same or equivalent component (element) is indexed with identical reference numeral.
As shown in Fig. 2, two layers of three chamber laminating systems described in the embodiment of the present invention, are included in two layers that vertical direction is arranged
Three cavity layer press mechanisms 4 and the input mechanism 5 and output mechanism 6 for being separately positioned on close two layers of three cavity layer press mechanisms, 4 both ends, two
Each layer of three cavity layer press mechanism of layer is equipped with evacuation and preliminary layer press fitting for laminated compenent product successively in the horizontal direction
Put, the solidification equipment for curing assembly product and cooling device (the first layer bag above for cooling component product
Include the first evacuation and preliminary laminater 7, the first solidification equipment 8 and the first cooling device 9；The underlying second layer includes the
Two evacuate and preliminary laminater 10, the second solidification equipment 11 and the second cooling device 12), the subassembly product of input mechanism 5 is defeated
Outlet is opposite with the evacuation of two layers three cavity layer press mechanisms 4 and the subassembly product input terminal of preliminary laminater, the group of output mechanism 6
Part product input terminal is opposite with the subassembly product output terminal of the cooling device of two layers of three cavity layer press mechanisms 4, two layers of three cavity layer press
Each layer of structure 4 is equipped with for evacuating the transmission assembly product between preliminary laminater, solidification equipment and cooling device
Transmission system, input mechanism 5 and output mechanism 6 be equipped with can lift to each layer of two layers of three cavity layer press mechanisms 4 and with
The transmission platform 13 of Transmission system docking in each layer.
Wherein, what " three chambers " in two layers of three cavity layer press mechanisms was signified is exactly to evacuate and preliminary laminater, solidification equipment
And cooling device.
In this example, the transmission of the transmission assembly product between preliminary laminater, solidification equipment and cooling device is being evacuated
System is circulation cloth.
In this example, input mechanism 5 and output mechanism 6 are equipped with the jacking system 14 for lifting the transmission platform 13,
Transmission platform 13 by the decelerating motor in jacking system 14 and elevating chain realize lifting with two layers three cavity layer press mechanisms 4
Transmission system docking in each layer.
Input mechanism 5 is used for the input of subassembly product, and the jacking system 14 in input mechanism 5 is used in input mechanism 5
The lifting of transmission platform 13, the subassembly product raising ensured from assembly line input are down to corresponding two layers of three cavity layer press mechanisms 4
First layer or the second layer；Input mechanism 5 mainly possesses the function of being docked with assembly line and evacuation and preliminary laminater, inputs machine
The input terminal of structure 5 is docked with assembly line, and the output terminal of input mechanism 5 is docked with evacuation and preliminary laminater, realization and flowing water
Line and evacuation and the stable automatic butt of preliminary laminater.
Evacuate and preliminary laminater is mainly used for vacuumizing and being tentatively laminated for subassembly product.As shown in figure 3, evacuate and
Preliminary laminater includes the upper operating mechanism that can be lifted and the lower operating mechanism below upper operating mechanism, upper working machine
Structure includes the upper table 15 with heating function and the upper offset plate 16 with the lower surface periphery airtight connection of upper table 15, under
Operating mechanism includes the lower table 17 with heating function, and the periphery of upper offset plate 16 is equipped with sealing structure 21；Upper operating mechanism
During decline, closed lamination chamber is formed between upper offset plate 16 and lower table 17；Shape between upper table 15 and upper offset plate 16
Into upper chamber.Thermocouple, quartz tube heater or resistance heater can be set in upper table and lower table, come
Realize the heating function of upper table and lower table.Since the upper table of the evacuation and preliminary laminater also has heating
Function, therefore, in addition to it can encapsulate the general components of solar cell, can also meet the special solar-electricity such as solar double-glass assemblies
The packaging technology requirement of pond component.
When being laminated, the subassembly product 17 that evacuation and preliminary laminater are entered by input mechanism is placed in lower work
On circulation cloth (Transmission system) on platform 17, upper operating mechanism declines, and subassembly product 18 is placed in closed lamination chamber,
By upper table 15 and the common heat effect of lower table 17, subassembly product 18 is heated, while lamination chamber is carried out
Vacuumize, the gas in subassembly product 18 is extracted out；Then, air is filled with into upper chamber makes upper offset plate 16 expand downward drum
Rise, offset plate 16 is close to subassembly product 18, subassembly product 18 is laminated；After the completion of action to be laminated, chamber is laminated
Inflation, upper operating mechanism's raising, subassembly product 18 enter solidification equipment by Transmission system (circulation cloth).
Solidification equipment and the structure of evacuation and preliminary laminater are essentially identical, and difference lies in the upper work of solidification equipment for it
There is no heating function as platform, only lower table has heating function, and solidification equipment is played to subassembly product (by evacuating and tentatively
Laminater is carried out after being tentatively laminated) carry out further lamination and cured effect.
The pressure that cooling device is mainly used for component quickly cools down.Cooling device and evacuation and the structure of preliminary laminater
Essentially identical, difference lies in the upper table of cooling device does not have heating function yet, and in the lower table of cooling device for it yet
There is circulating water to make it have refrigerating function in portion, is held down assembly product by the upper offset plate of upper table, makes subassembly product tight
Lower table is pasted, realizes the purpose to subassembly product fast cooling.
Output mechanism 6 is mainly used for the output of subassembly product, and the jacking system 14 in output mechanism 6 is used for output mechanism 6
In transmission platform 13 lifting, ensure output mechanism 6 docked with the first layer in two layers of three cavity layer press mechanisms 4 or the second layer,
Output mechanism mainly possesses the function of being docked with cooling device and assembly line, and the input terminal of output mechanism is docked with cooling device,
The output terminal of output mechanism is docked with assembly line, is realized and assembly line and the stable automatic butt of cooling device.
In this example, each layer of two layers of three cavity layer press mechanisms can pass through electric control system independent control.Two layers of three chambers
Evacuation and preliminary laminater, solidification equipment and cooling device in each layer of laminate mechanism can pass through electric control system
Independent control.It so can increase substantially the flexibility of the laminating system, also drastically increase production efficiency.
In this example, two ends of two layers of three cavity layer press mechanisms 4 are equipped with cleaning systems 19.Cleaning systems can be to circulation
Cloth (Transmission system) is cleaned, and prevents subassembly product to be contaminated.
In this example, set between each layer of evacuation of two layers three cavity layer press mechanisms 4 and preliminary laminater and solidification equipment
There is transition heating module 20.It can be made from the component evacuated and preliminary laminater preliminary layer presses out by transition heating module
Product improves the quality and performance of subassembly product to that will not cool down during solidification equipment.
The course of work of two layers of three chamber laminating systems described in the present embodiment is as follows：The jacking system 14 of input mechanism 5 will
Transmission platform 13 is adjusted to height is docked with assembly line, and subassembly product enters input mechanism 5, input mechanism from pipeline
The first layer position that 5 jacking system 14 adjusts transmission platform 13 to two layers of three cavity layer press mechanisms is (above for first
Layer), and docked with the first evacuation and preliminary laminater 7, the subassembly product on transmission platform 13 is passed through into Transmission system (circulation
Cloth) the first evacuation and preliminary laminater 7 are transmitted to, first evacuates with preliminary laminater 7 according to technique initialization parameter, carries out
It is full-automatic to evacuate and the cured process of preliminary layer；After the process, subassembly product enters the by Transmission system (circulation cloth)
One solidification equipment 8, the first solidification equipment 8 complete automatic lamination process according to technique initialization parameter, realize to subassembly product into
One step is laminated and cures；After the process, subassembly product enters the first cooling device 9 by Transmission system (circulation cloth), presses
Subassembly product is forced according to technique initialization parameter quickly to cool down, after the process, the jacking system 14 of output mechanism 6 carries
Preceding adjust transmission platform 13 to first layer position, the transmission platform 13 of output mechanism 6 is docked with the first cooling device 9, by
The subassembly product in Transmission system (circulation cloth) in one cooling device 9 is transmitted to the transmission platform 13 of output mechanism 6, finally,
Output mechanism 6 is docked with assembly line, and subassembly product enters assembly line and realizes discharging, completes whole lamination process.
The course of work of the second layer of two layers of three chamber laminating systems is identical with the course of work of first layer, and two layers
Between be independent control, input mechanism and output mechanism can coordinate two layers of respective work rhythm, carry out subassembly product
Output and input, first layer and the second layer can work independently at the same time, non-interference.Substantially increase the flexible of the laminating system
Property, production capacity is drastically increased, has saved work-yard, has saved cost.
The description above presented to the specific illustrative embodiment of the present invention is in order at the purpose of illustration and description.Above
Description be not intended to become milli exhaustively, be not intended to limit the invention to disclosed precise forms, it is clear that root
All it is possible according to many change and variations of above-mentioned teaching.It is to explain this hair to select illustrative embodiments and be described
Bright certain principles and its practical application, so that others skilled in the art can realize and utilize each of the present invention
Kind illustrative embodiments and its various selection forms and modification.The scope of the present invention be intended to by the appended claims and
Its equivalents is limited.
Claims (11)
1. a kind of three chamber laminating system of multilayer, it is characterised in that including three cavity layer press mechanism of multilayer and be separately positioned on close
The input mechanism and output mechanism at the three cavity layer press mechanism both ends of multilayer, each layer of the three cavity layer press mechanism of multilayer according to
It is secondary to be equipped with the evacuation for laminated compenent product with preliminary laminater, the solidification equipment for curing assembly product and for cold
But the cooling device of subassembly product, the evacuation of the subassembly product output terminal of the input mechanism and the three cavity layer press mechanism of multilayer
It is opposite with the subassembly product input terminal of preliminary laminater, the subassembly product input terminal of the output mechanism and three chamber of multilayer
The subassembly product output terminal of the cooling device of laminate mechanism is opposite, and each layer of the three cavity layer press mechanism of multilayer, which is equipped with, to be used for
The transmission system of transmission assembly product between the evacuation and preliminary laminater, the solidification equipment and the cooling device
System, the input mechanism and the output mechanism be equipped with can lift to each layer of the three cavity layer press mechanism of multilayer and with
The transmission platform of Transmission system docking in each layer.
2. three chamber laminating system of multilayer according to claim 1, it is characterised in that the three cavity layer press mechanism of multilayer it is every
One layer is independent control.
3. three chamber laminating system of multilayer according to claim 1, it is characterised in that the three cavity layer press mechanism of multilayer it is every
The evacuation and preliminary laminater, the solidification equipment and the cooling device in one layer are independent control.
4. three chamber laminating system of multilayer according to claim 1, it is characterised in that the end of the three cavity layer press mechanism of multilayer
Portion is equipped with cleaning systems.
5. three chamber laminating system of multilayer according to claim 1, it is characterised in that the three cavity layer press mechanism of multilayer it is every
Transition heating module is equipped between one layer of the evacuation and preliminary laminater and the solidification equipment.
6. three chamber laminating system of multilayer according to claim 1, it is characterised in that the input mechanism and the output machine
Structure is equipped with the jacking system for lifting the transmission platform, and the transmission platform passes through the deceleration electricity in the jacking system
Machine and elevating chain realize lifting to be docked with the Transmission system in each layer of the three cavity layer press mechanism of multilayer.
7. three chamber laminating system of multilayer according to claim 1, it is characterised in that the evacuation and preliminary laminater bag
The upper operating mechanism that can be lifted and the lower operating mechanism below the upper operating mechanism are included, the upper operating mechanism includes
Upper table with heating function and the upper offset plate with the lower surface periphery airtight connection of the upper table, the lower work
Mechanism includes the lower table with heating function, and the periphery of the upper offset plate is equipped with sealing structure.
8. three chamber laminating system of multilayer according to claim 7, it is characterised in that when the upper operating mechanism declines, institute
State and closed lamination chamber is formed between offset plate and the lower table.
9. three chamber laminating system of multilayer according to claim 7, it is characterised in that the upper table and the upper offset plate
Between form upper chamber.
10. three chamber laminating system of multilayer according to claim 1, it is characterised in that be included in the two of vertical direction arrangement
Three cavity layer press mechanism of layer, each layers of two layers of three cavity layer press mechanisms have been sequentially arranged the evacuation and preliminary in the horizontal direction
Laminater, the solidification equipment and the cooling device.
11. a kind of application method of laminating system, it is characterised in that the laminating system is described in claim any one of 1-10
Three chamber laminating system of multilayer, which includes step in detail below：
1) input mechanism adjusts transmission platform to height is docked with assembly line, and subassembly product enters input from pipeline
Mechanism, input mechanism adjust transmission platform to wherein one layer of position of three cavity layer press mechanism of multilayer, and with the evacuation of this layer and just
Laminater docking is walked, subassembly product is transmitted to the evacuation of this layer and preliminary laminater, the evacuation of this layer and preliminary lamination
Device carries out full-automatic evacuate and the cured process of preliminary layer according to technique initialization parameter；
2) subassembly product enters the solidification equipment of this layer by Transmission system, the solidification equipment of this layer according to technique initialization parameter,
Complete further lamination and solidification process；
3) subassembly product enters the cooling device of this layer by Transmission system, subassembly product is carried out according to technique initialization parameter strong
The quick cooling of system；
4) output mechanism in advance adjusts transmission platform to this layer of position, the transmission platform of output mechanism and the cooling device of this layer
Docking, subassembly product is transmitted to the transmission platform of output mechanism, finally, output mechanism is docked with assembly line, subassembly product into
Enter assembly line and realize discharging, complete whole lamination process.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711187826.3A CN107962851A (en) | 2017-11-24 | 2017-11-24 | Three chamber laminating system of multilayer and its application method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711187826.3A CN107962851A (en) | 2017-11-24 | 2017-11-24 | Three chamber laminating system of multilayer and its application method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107962851A true CN107962851A (en) | 2018-04-27 |
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ID=62000537
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711187826.3A Pending CN107962851A (en) | 2017-11-24 | 2017-11-24 | Three chamber laminating system of multilayer and its application method |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109130449A (en) * | 2018-09-17 | 2019-01-04 | 汉能移动能源控股集团有限公司 | Rotary lamination packaging system and lamination processing method |
| CN109192820A (en) * | 2018-10-29 | 2019-01-11 | 河北羿珩科技有限责任公司 | Multi-Layer and Multi-Cavity laminating system and its application method |
| CN110676335A (en) * | 2019-10-01 | 2020-01-10 | 秦皇岛博硕光电设备股份有限公司 | Hot-pressing curing method for photovoltaic module and pressing equipment for hot-pressing curing |
| CN113263820A (en) * | 2021-05-19 | 2021-08-17 | 曹健 | Composite construction iron powder core idiosome piles up even suppression device |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201423790Y (en) * | 2009-04-28 | 2010-03-17 | 秦皇岛瑞晶太阳能科技有限公司 | Rubber sheet type packaging platform for solar battery module laminator |
| CN202573212U (en) * | 2012-05-08 | 2012-12-05 | 秦皇岛瑞晶太阳能科技有限公司 | Laminating machine of cooling-type three-cavity energy-saving solar cell module |
| CN104827742A (en) * | 2014-09-10 | 2015-08-12 | 安阳高新区生产力促进中心 | Laminating machine and laminating process of photovoltaic assembly |
| CN105128492A (en) * | 2015-08-25 | 2015-12-09 | 武汉三工光电设备制造有限公司 | Multilayered laminating machine for solar battery assemblies |
| CN105500887A (en) * | 2016-01-15 | 2016-04-20 | 河北羿珩科技股份有限公司 | Three-cavity linkage type laminator special for double glass assemblies |
| CN205439498U (en) * | 2015-12-15 | 2016-08-10 | 河北羿珩科技股份有限公司 | Double -deck two -chamber formula solar module laminator |
| CN206254607U (en) * | 2016-10-05 | 2017-06-16 | 秦皇岛可视自动化设备有限公司 | A kind of three chamber solar module laminating machinees |
| CN107215074A (en) * | 2017-04-01 | 2017-09-29 | 秦皇岛可视自动化设备有限公司 | A kind of method of new plate-like piece laminating machine and laminated plate-shaped part |
| CN207509931U (en) * | 2017-11-24 | 2018-06-19 | 河北羿珩科技有限责任公司 | Three chamber laminating system of multilayer |
-
2017
- 2017-11-24 CN CN201711187826.3A patent/CN107962851A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201423790Y (en) * | 2009-04-28 | 2010-03-17 | 秦皇岛瑞晶太阳能科技有限公司 | Rubber sheet type packaging platform for solar battery module laminator |
| CN202573212U (en) * | 2012-05-08 | 2012-12-05 | 秦皇岛瑞晶太阳能科技有限公司 | Laminating machine of cooling-type three-cavity energy-saving solar cell module |
| CN104827742A (en) * | 2014-09-10 | 2015-08-12 | 安阳高新区生产力促进中心 | Laminating machine and laminating process of photovoltaic assembly |
| CN105128492A (en) * | 2015-08-25 | 2015-12-09 | 武汉三工光电设备制造有限公司 | Multilayered laminating machine for solar battery assemblies |
| CN205439498U (en) * | 2015-12-15 | 2016-08-10 | 河北羿珩科技股份有限公司 | Double -deck two -chamber formula solar module laminator |
| CN105500887A (en) * | 2016-01-15 | 2016-04-20 | 河北羿珩科技股份有限公司 | Three-cavity linkage type laminator special for double glass assemblies |
| CN206254607U (en) * | 2016-10-05 | 2017-06-16 | 秦皇岛可视自动化设备有限公司 | A kind of three chamber solar module laminating machinees |
| CN107215074A (en) * | 2017-04-01 | 2017-09-29 | 秦皇岛可视自动化设备有限公司 | A kind of method of new plate-like piece laminating machine and laminated plate-shaped part |
| CN207509931U (en) * | 2017-11-24 | 2018-06-19 | 河北羿珩科技有限责任公司 | Three chamber laminating system of multilayer |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109130449A (en) * | 2018-09-17 | 2019-01-04 | 汉能移动能源控股集团有限公司 | Rotary lamination packaging system and lamination processing method |
| CN109192820A (en) * | 2018-10-29 | 2019-01-11 | 河北羿珩科技有限责任公司 | Multi-Layer and Multi-Cavity laminating system and its application method |
| CN109192820B (en) * | 2018-10-29 | 2024-04-05 | 河北羿珩科技有限责任公司 | Multilayer multichamber lamination system and method of using same |
| CN110676335A (en) * | 2019-10-01 | 2020-01-10 | 秦皇岛博硕光电设备股份有限公司 | Hot-pressing curing method for photovoltaic module and pressing equipment for hot-pressing curing |
| CN113263820A (en) * | 2021-05-19 | 2021-08-17 | 曹健 | Composite construction iron powder core idiosome piles up even suppression device |
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