CN105172305B - The solar components laminater and its laminating method of a kind of many counterweights - Google Patents

The solar components laminater and its laminating method of a kind of many counterweights Download PDF

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Publication number
CN105172305B
CN105172305B CN201510652102.6A CN201510652102A CN105172305B CN 105172305 B CN105172305 B CN 105172305B CN 201510652102 A CN201510652102 A CN 201510652102A CN 105172305 B CN105172305 B CN 105172305B
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China
Prior art keywords
axis
counterweight
press
component
solar
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CN201510652102.6A
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Chinese (zh)
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CN105172305A (en
Inventor
刘胜荣
施云贵
蔡康松
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Huangshan University
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Huangshan University
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Publication of CN105172305A publication Critical patent/CN105172305A/en
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Publication of CN105172305B publication Critical patent/CN105172305B/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/0046Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by constructional aspects of the apparatus
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • B32B37/1018Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure using only vacuum

Abstract

The present invention provides a kind of solar components laminater of many counterweights, including:Body, upper lid, upper lid cooperatively forms with body sealing and the solar energy layer pressing plate for being used for being laminated solar cell module is provided with chamber, upper lid, wherein, the lower chambers for accommodating solar cell module are formed between solar energy layer pressing plate and body, upper chamber is formed between solar energy layer pressing plate and upper lid;Solar components laminater also includes many counterweight press devices for being used to press lid, many counterweight press devices are installed on the top of lid, X-axis moving parts, the Z axis moving parts for driving press component to be moved along Z axis including press component, for driving press component to move along the x-axis, press component is installed on the Z axis moving parts, and Z axis moving parts are installed on X-axis moving parts.The laminating method of above-mentioned solar components laminater is also provided.The solar components laminater of the present invention can effectively lift the binding ability between solar cell module.

Description

The solar components laminater and its laminating method of a kind of many counterweights
Technical field
The present invention relates to a kind of solar cell module manufacturing equipment field, more particularly to a kind of solar energy group of many counterweights Part laminater and its laminating method.
Background technology
With the growing of industrial circle and progress, it is non-renewable that the energy more they tends to anxiety, particularly coal, oil etc. The increasingly reduction of the energy, is impacted, for example using the application field of the above-mentioned energy:In field of traffic, because the rise of oil price, Thus the contradiction of every aspect has been triggered, the thus exploitation of new energy seems more and more urgent with application, and solar energy is as new Renewable resource, is widely studied in recent years.
Solar cell module (also referred to as " photovoltaic module ") be some cells are gone here and there according to electrical property classification, Parallel connection, is combined into the minimum unit that independently can be used as power supply after encapsulation.Solar cell module has various Size and dimension, conventional solar cell module structure is followed successively by glass/eva film/solar cell/EVA from top to bottom Film/TPT back veneer materials.
The manufacture method of above-mentioned solar cell module generally includes following several steps:
1st, some solar cells are welded as a whole with the mutual latticing prepared;
2nd, solar battery array, EVA, the TPT formed from bottom to top by glass, EVA, through series and parallel is superimposed together It is put into solar components laminater;
3rd, the upper and lower chamber of laminater is vacuumized using vacuum layer platen press, heats, pressurizes, by glass, EV films, too Positive energy array, EVA, TPT hot pressing together, are taken out after shaping.
4th, install terminal box additional and solar cell module is made in power line.
In the manufacturing process of solar cell module, lamination is one of very important process, is related to solar-electricity The performance and service life of pond component, thus solar components laminater and its laminating method are proposed it is very high will Ask, however, existing solar energy layer pressure device and its laminating method due to be short of the heating to upper and lower chamber, vacuum and There is crackle, bubble in the strict control of moulding pressure etc., made solar cell module, and solar cell module Binding ability is poor.
The content of the invention
The present invention is in order to solve solar components laminater of the prior art and its sun made by laminating method There is the poor technical problem of bubble, binding ability in energy battery component.
The invention provides a kind of solar components laminater of many counterweights, including:Body, openable it is installed on institute The upper lid on body is stated, the upper lid cooperatively forms to be provided with chamber, the upper lid with body sealing to be used to be laminated solar-electricity The solar energy layer pressing plate of pond component, wherein, formed between solar energy layer pressing plate and body for accommodating solar cell module Lower chambers, upper chamber is formed between solar energy layer pressing plate and upper lid;The solar components laminater also includes being used to press Many counterweight press devices of upper lid, many counterweight press devices are installed on the top of lid, including press component, for driving X-axis moving parts that the press component is moved along the x-axis, the Z axis exercise group for driving the press component to be moved along Z axis Part, the press component is installed on the Z axis moving parts, and the Z axis moving parts are installed on X-axis moving parts On.
The present invention also provides a kind of laminating method of the solar components laminater of many counterweights, comprises the steps:
S1, solar cell module to be laminated is put into lower chambers;
S2, vacuumize:First lower chambers are vacuumized, then upper and lower chamber vacuumized simultaneously;
S3, mechanical lamination process:Many counterweight press devices are pressed upper lid, then pass through solar energy laminated compenent The solar cell module of bottom chamber is pressurizeed, while being heated to lower chambers;
S4, by after lamination solar cell module take out.
The solar components laminater that the present invention is provided is by setting many counterweight press devices to realize to solar-electricity The mechanical lamination of pond component, and the pneumatic type to solar cell module is preferably also realized by setting vacuum plant Lamination, so as to make the bubble between solar cell module smoothly discharge, improves the solar cell module after lamination Between binding ability, and the present invention solar components laminater be widely used, be conducive to the hair of existing solar cell Exhibition.
Brief description of the drawings
Fig. 1 is the schematic diagram for the solar components laminater that the present invention is provided.
Fig. 2 is that the upper lid of the solar components laminater shown in Fig. 1 is in the schematic diagram of opening.
Fig. 3 is that the upper lid of the solar components laminater shown in Fig. 1 is in the schematic diagram of closed mode.
Fig. 4 is partial sectional views of the Fig. 2 along A-A directions.
Fig. 5 is partial sectional views of the Fig. 3 along B-B directions.
Fig. 6 is the sectional view of the upper lid shown in Fig. 4.
Fig. 7 is the schematic diagram of the vacuum system for the solar components laminater that the present invention is provided.
Fig. 8 is the schematic perspective view of the counterweight press device for the solar components laminater that the present invention is provided.
Fig. 9 is the front schematic view of the counterweight press device shown in Fig. 8.
Figure 10 is the side schematic view of the counterweight press device shown in Fig. 8.
Figure 11 is the schematic perspective view of the press component shown in Fig. 8.
Figure 12 is the schematic perspective view of another angle of the press component shown in Figure 11.
Figure 13 is the schematic perspective view of a part for the press component shown in Figure 11, and that removes fixed plate.
Figure 14 is the schematic perspective view of one group of counterweight component shown in Figure 11 and a main pressing piece.
Figure 15 is the decomposing schematic representation of the main pressing piece shown in Figure 11.
Figure 16 is the schematic perspective view of the Y-axis guide of the press component shown in Figure 11.
Figure 17 is the schematic perspective view of the X-axis guide of the press component shown in Figure 11.
Figure 18 is the decomposing schematic representation of the auxiliary pressing piece of the press component shown in Figure 11.
Embodiment
The embodiment of the present invention is further detailed below in conjunction with accompanying drawing.Below in conjunction with accompanying drawing to this hair Bright embodiment is further detailed.
Deposited the invention aims to the solar cell module for overcoming existing solar components laminater to make In the poor shortcoming of bubble, binding ability there is provided a kind of solar components laminater of many counterweights, to realize to solar-electricity The mechanical lamination of pond component and pneumatic type lamination.
As Figure 1-3, the solar energy layer pressure device of many counterweights of the invention, including:Laminater body 1, upper lid 2, The upper lid 2 is openable to be installed on the body 1;The body 1 is provided with cylinder actuator 10, and the cylinder is performed Mechanism 10 is connected with upper lid 2 and controls the upper lid 2 relative to the closure or openness of body 1.
Refering to Fig. 4 and Fig. 5, the upper lid 2 cooperatively forms to be provided with chamber, the upper lid 2 with the sealing of body 1 to be used to be laminated The solar energy layer pressing plate 4 of solar cell module, wherein, formed between solar energy layer pressing plate 4 and body 1 for accommodating solar energy The lower chambers 6 of battery component, form upper chamber 5 between solar energy layer pressing plate 4 and upper lid 2.
Specifically, refering to Fig. 6, the upper lid 2 includes pressing on the first top board 21, the second top board 22, described first The lower groove 24 provided with insertion second top board 22 in upper groove body 23, second top board 22 is provided with plate 21;It is described too Positive energy laminate 4 is seal-installed between the top board 22 of the first top board 21 and second, solar energy layer pressing plate 4 and upper lid 2 Between form the upper chamber 5.Refering to Fig. 2 and Fig. 5, the body 1 includes support 11, the heating plate being installed on support 11 12 and the lower platen 13 for being used to place solar cell module of the top of heating plate 12 is installed on, the solar energy layer pressing plate 4 The lower chambers 6 are formed between lower platen 13.
Refering to Fig. 2, heating plate 12 is provided with the oil circuit 14 for being used for heating lower platen 13, and the oil circuit 14 connection hot oil pump simultaneously leads to Die heater progress temperature control (not shown) is crossed, die heater is -190 DEG C of room temperature to the temperature adjustment of heating plate 12;Due to pushing Plate 13 is in contact with heating plate 12, and the heat of heating plate 12 can heat the solar energy lamination group in lower chambers 6 by top board 13 Part.The heating plate 12, oil circuit 14 and die heater can be achieved by the prior art, and be mainly used in entering solar cell module Row heating, will not be described here.
In a preferred embodiment of the invention, the solar components laminater of many counterweights also provides a kind of vacuum system 3, Coordinate to realize to solar cell module for realizing the vacuum control to upper and lower chamber 5,6, and with solar energy layer pressing plate 4 Pneumatic type lamination, the vacuum system 3 can use existing solar components laminater vacuum system, as shown in fig. 7, In a preferred embodiment, vacuum system 3 include be used for upper and lower chamber 5,6 is vacuumized vavuum pump 31, be connected to upper and lower chamber Upper and lower vacuum line 51,61 (referring to Fig. 2,3) between room 5,6 and vavuum pump 31.Wherein, vavuum pump 31 of the invention can be with It it is one or multiple.Specifically, the upper chamber 5 is provided with upper vacuum line 51, the free end of upper vacuum line 51 Peace on vavuum pump 31, upper vacuum line 51 is connected provided with upper vacuum interface 59 (referring to Fig. 2), and by the upper vacuum interface 59 Equipped with upper chamber vent valve 52 and upper chamber vacuum valve 53, upper chamber vacuum valve 53 is used to vacuumize upper chamber 5, upper chamber vent valve 52 are used to be passed through air into upper chamber 5, and upper chamber 5 is combined by upper chamber vacuum valve 53 and upper chamber vent valve 52 and controls its vacuum Degree.The control device of the vacuum system 3 of the present invention is controller 32, for realizing automatically controlling for vacuum system 3, and it controls electricity Road part can be achieved by the prior art, and the setting of each parameter can be set according to user to be completed, so as to realize oneself of laminating technology Dynamicization is operated.Upper chamber vacuum meter 54, upper chamber vacuum pressure sensor 55 and upper chamber are also equipped with the upper vacuum line 51 Vacuum solenoid 56, the upper chamber vacuum solenoid 56 is in series and is combined into one with upper chamber vent valve 52, collectively constitutes and puts The executing agency of gas operation, unlatching, closing and opening degree that can be by adjusting upper chamber vacuum solenoid 56 control whether to deflate And the speed deflated, upper chamber vacuum pressure sensor 55, upper chamber vacuum solenoid 56 are electrically connected to form a control with controller 32 System processed, upper chamber vacuum pressure sensor 55 controls the pressure signal transmission of upper chamber 5 to controller 32, and by controller 32 Upper chamber vacuum solenoid 56 is turned on and off, so as to realize the control to the stage deflation of upper chamber 5.For example:When user is in control Set on device 32 processed when being deflated to a certain desired value to upper chamber 5, the control upper chamber of controller 32 vacuum solenoid 56 is opened, until When the pressure value for feeding back to controller 32 of upper chamber vacuum pressure sensor 55 reaches desired value, controller 32 closes upper chamber vacuum Magnetic valve 56, this stage deflation terminates.
Similarly, lower chambers 6 are provided with lower vacuum line 61, and the free end of lower vacuum line 61 is provided with lower vacuum interface 69 (referring to Fig. 2), and vavuum pump 31 is connected by the lower vacuum interface 66, for being vacuumized in the course of work to lower chambers 6, under Lower room vent valve 62 and lower room vacuum valve 63 are installed, lower room vacuum valve 63 is used to take out lower chambers 6 on vacuum line 61 Vacuum, lower room vent valve 62 is used to be passed through air into lower chambers 6, and lower chambers 6 are by lower room vacuum valve 63 and lower room vent valve 62 Combination controls its vacuum, be also equipped with the lower vacuum line 61 lower room vacuum meter 64, lower room vacuum pressure sensor 65, Lower room vacuum solenoid 66, the lower room vacuum solenoid 66 is in series and is combined into one with lower room vent valve 62, common group Into the executing agency of bleed air operation, lower room vacuum pressure sensor 65, lower room vacuum solenoid 66 are electrically connected with controller 32, under The pressure signal transmission of lower chambers 6 is controlled lower room vacuum by room vacuum pressure sensor 65 to controller 32, and by controller 32 Magnetic valve 66 is turned on and off, so that the control deflated to lower chambers 6 can be realized.
It is noted that solar energy layer pressing plate 4 of the present invention can be known to the skilled person it is various Flexible member, and need with certain heat resistance, for example:Heat resistant rubber can be used.Solar energy layer pressing plate 4 is arranged at lid 2 On, it is placed between upper groove body 23 and lower groove 24 forming upper chamber 5 and lower chambers 6, when the air pressure of upper chamber 5 is more than lower chambers During 6 air pressure, solar energy layer pressing plate 4 produces deformation, and the solar cell module being pointed in lower chambers 6 produces certain layer Pressure pressure, so as to realize the lamination to solar cell module product.The usual thickness of solar energy layer pressing plate 4 is 4~5mm, at this In embodiment, its shrinkage factor can reach 550% to 800%, and solar energy layer pressing plate 4 plays important work in whole laminating apparatus With price costly, when mounted needs to be installed to tensioned state, when otherwise, taking out, putting vacuum, and solar energy layer pressing plate 4 can not The dynamics for pushing down solar cell module or pressure completely is not big enough, between solar cell module (especially in eva film Bubble) cannot squeeze out completely, the adhesion strength of (especially eva film and glass plate) between solar cell module Requirement is not reached.
The solar components laminater for theing improvement is that many counterweights of the present invention also includes many counterweight press devices 100, to realize the mechanical lamination to solar cell module, many counterweight press devices 100 of the invention are installed on lid 2 Top, for pressing upper lid 2, the upper lid 2 is made of elastomeric material, upper chamber 5 is compressed in pressing during lid 2, so that the sun Energy laminate 4 produces deformation, and the solar cell module being pointed in lower chambers 6 produces lamination pressure.Described many counterweights Press device 100 can realize the pressing to the upper diverse location of lid 2, and pressing force is adjustable so as to solar battery group Needed for the dynamics that part applies meets solar cell, and many counterweight press devices 100 can upper lid 2 diverse location Bubble in pressing, convenient extrusion solar cell module, results in adhesion strength preferably solar cell module.
It is noted that upper lid 2 of the present invention needs the various elasticity members being known to the skilled person Part, and need with certain heat resistance, for example:Heat resistant rubber can be used.So as to be covered when in the pressing of many counterweight press devices 100 When 2, the upper stress of lid 2 is pushed, and because solar energy layer pressing plate 4 is arranged on upper lid 2, is placed between upper groove body 23 and lower groove 24 Upper chamber 5 and lower chambers 6 are formed, when the air pressure of upper chamber 5 is more than the air pressure of lower chambers 6, solar energy layer pressing plate 4 produces shape Become, and the solar cell module being pointed in lower chambers 6 produces certain lamination pressure, so as to realize to solar battery group The mechanical lamination of part product.
Specifically, as seen in figs. 8-10, described many counterweight press devices 100 include press component 7, for driving State X-axis moving parts 8, the Z axis exercise group for driving the press component 7 to be moved along Z axis that press component 7 is moved along the x-axis Part 9, the press component 7 is installed on the Z axis moving parts 9, and the Z axis moving parts 9 are installed on X-axis exercise group On part 8;The press component 7 includes mounting bracket 71, array counterweight component 70 and several main pressings for pressing upper lid 2 Part 72, the mounting bracket 71 is installed on Z axis moving parts 9, and the array counterweight component 70 is fixed on mounting bracket 71, described Several main pressing pieces 72 are correspondingly arranged and are connected with the array counterweight component 70 respectively.Press component 7 passes through X-axis exercise group Part 8, the driving of Z axis moving parts 9 and can be moved along X-direction and Z-direction, press component 7 moves to move along X-direction To at the diverse location of upper lid 2, press component 7 is moved along Z axis to press upper lid 2, so as to pass through upper lid 2, solar energy layer Pressure component 4 presses to each position of solar cell module.The press component 7 include array counterweight component 70, with And several main pressing pieces 72, main pressing piece 72 presses down on lid 2 under the driving of Z axis moving parts, due to the different sun Pressing force needed for energy battery component is different, when the pressing force needed for solar cell module is not above the bullet of main pressing piece 72 Property power when, main pressing piece 72 lid 2 in elasticity pressing in the range of the elastic force, when the pressing force needed for solar cell module exceedes During the elastic force of main pressing piece 72, then main pressing piece 72 leans counterweight component 70 upwards, then now counterweight component 70 works, and leads to Appropriate gravity can be applied to main pressing piece 72 by crossing counterweight component 70 so that main pressing piece 72 can be with solar cell module The required upper lid 2 of pressing force pressing, so as to be pressed to solar cell module, the dynamics of lid 2 is in certain model in pressing Enclose it is interior effectively automatically adjusted, the precision of pressing is high, can be applicable to a variety of solar-electricities of different pressing forces Pond component, it is applied widely.
Specifically, as shown in Fig. 8 to Figure 10, the Z axis moving parts 9 include Z axis movable plate 91, located at Z axis movement At least one Z axis guide rail 92, Z axis drive belt 93 on plate 91 and the Z axis for driving the shuttling movement of Z axis drive belt 93 Drive motor 94, wherein, Z axis drive motor 94 is one or two, is connected to one end or two of Z axis drive belt 93 End, in the present embodiment, the Z axis drive motor 94 are one, are connected to one end of Z axis drive belt 93, press component 7 is pacified Loaded in Z axis guide rail 92, and be connected with Z axis drive belt 93, under the driving of Z axis drive motor 94, press component 7 by Z axis drive belt 93 drives, and is slided along Z axis guide rail 92.Press component 7 is driven to be moved along Z axis by Z axis moving parts 9, can Realization presses down on lid 2, is upwardly away from lid 2, so that press component 7 can press lid 2, is further advanced by too Positive energy laminate 4 presses to solar cell module.
Similarly, as shown in Fig. 8 to Figure 10, the X-axis moving parts 8 include X-axis movable plate 81, located at X-axis movable plate At least one X-axis guide rail 82, X-axis drive belt 83 on 81 and for driving the X-axis of the shuttling movement of X-axis drive belt 83 to drive Dynamic motor 84, wherein, X-axis drive motor 84 is one or two, is connected to one end or two ends of X-axis drive belt 83, In the present embodiment, the X-axis drive motor 84 is one, is connected to one end of X-axis drive belt 83, Z axis moving parts 9 with And be installed on the integral installation of press component 7 on Z axis moving parts 9 in X-axis guide rail 82, and with the phase of X-axis drive belt 83 Connection, under the driving of X-axis drive motor 84, Z axis moving parts 9 and press component 7 are driven by X-axis drive belt 83, along X-axis Guide rail 82 is slided.X-axis moving parts 8 are used to drive press component 7 to move along the x-axis so that press component 7 can be on being moved to At the diverse location of lid 2, so that press component 7 can press the diverse location of lid 2, so as to solar cell module Diverse location is pressed.
In a preferred embodiment of the invention, as shown in Fig. 8 to 15, as noted earlier, the press component 7 includes peace 71, array counterweight component 70 and several main pressing pieces 72 for pressing upper lid 2 are shelved, the mounting bracket 71 is installed on Z axis On moving parts 9, the array counterweight component 70 is fixed on mounting bracket 71, several main pressing pieces 72 respectively with the number Group counterweight component 70 is fixedly connected.In the present embodiment, the press component 7 includes four groups of counterweight components 70 and four masters press Casting die 72, can be pressed upper lid 2, and then solar cell module is pressed simultaneously.By setting above-mentioned X-axis exercise group Part 8 and Z axis moving parts 9 can realize that press component 7 is moved along X-axis, Z axis, and regulation press component 7 is in X-axis and Z-direction Position, further, press component 7 includes array counterweight component 70 and being correspondingly arranged simultaneously with the array counterweight component 70 The several main pressing pieces 72 being connected, the Z axis moving parts 9 can drive press component 7 overall downwards close to upper lid 2, main Pressing piece 72 presses down on lid 2 under the driving of Z axis moving parts 9, due to pressing needed for different solar cell modules Pressure is different, and when the pressing force needed for upper lid 2 is not above the elastic force of main pressing piece 72, main pressing piece 72 is in elastic force model The interior upper lid 2 of elasticity pressing is enclosed, when the pressing force needed for solar cell module exceedes the elastic force of main pressing piece 72, then master presses Casting die 72 leans counterweight component 70 upwards, then now counterweight component 70 works, and can apply appropriate by counterweight component 70 Gravity gives main pressing piece 72 so that main pressing piece 72 can be with the upper lid 2 of pressing force pressing needed for solar cell module, example Such as:Pressing force needed for solar cell module there may be difference, and every kind of solar cell module needs certain press Pressure, the pressing force is bonded together required dynamics, those skilled in the art for each component of solar cell module It should be understood that if the pressing force of the upper lid 2 of pressing is too small, the dynamics applied to solar cell module is inadequate, solar-electricity The bubble of (bubble especially in eva film) cannot be squeezed out completely between the component of pond, between solar cell module The adhesion strength of (especially eva film and glass plate) does not reach requirement.If the pressing force of lid 2 is excessive in pressing, on the one hand It is possible to damage lid 2, on the other hand also effectively solar cell module can not be pressed.In the present embodiment, it is main Pressing piece 72 presses down on lid 2 under the driving of Z axis moving parts 9, main pressing piece 72 can its spring elastic force model Enclose it is interior elastic force is applied to upper lid 2, when the pressing force needed for upper lid 2 exceeds the elastic force of main pressing piece 72, then main pressing piece 72 lean counterweight component 70 upwards, and now counterweight component 70 works, by counterweight component 70 can apply appropriate gravity to Main pressing piece 72 so that main pressing piece 72 can be with the upper lid 2 of pressing force pressing needed for solar cell module.
Specifically, in the first preferred embodiment of the present invention, as shown in Figure 11 to 14, the press component 7 Mounting bracket 71 includes fixed plate 711, the fixed block 712 and spacer block 713 being installed in fixed plate 711, the He of spacer block 713 Fixed block 712 is installed in fixed plate 711, and fixed block 712 is located at the lower end of fixed plate 711, and spacer block 713 is located at fixed block 712 Top.The fixed plate 711 is fixed on Z axis moving parts 9, in the present embodiment, refering to Fig. 8, and the fixed plate 711 is pacified Loaded on Z axis moving parts 9, so that press component 7 is integrally fastened on Z axis moving parts 9.
As shown in Fig. 8 to Figure 14, in the present embodiment, every group of counterweight component includes the in four groups of counterweight components 70 One counterweight component 701 and the second counterweight component 702, refering to Figure 13 to Figure 15, the first counterweight component 701 includes first respectively Counterweight package traces 7011, the first counterweight sliding block 7012, the first counterweight mounting seat being fixedly connected with the first counterweight sliding block 7012 7013, and the first counterweight 7014 being installed in the first counterweight mounting seat 7013, the first counterweight package traces 7011 are pacified Loaded in fixed plate 711, the first counterweight sliding block 7012 is installed in the first counterweight package traces 7011 and along the first counterweight Package traces 7011 are moved up and down, and the first counterweight mounting seat 7013 of the main pressing piece 72 and the first counterweight component 701 is fixed Connect and be located at the lower section of the first counterweight 7014.Similarly, refering to Figure 13 and Figure 14, the second counterweight component 702 is wrapped respectively Include the second counterweight package traces 7021, the second counterweight sliding block 7022, the second counterweight being fixedly connected with the second counterweight sliding block 7022 Mounting seat 7023, and the second counterweight 7024 being installed in the second counterweight mounting seat 7023, the second counterweight package traces 7021 are installed in fixed plate 711, and the second counterweight sliding block 7022 is installed in the second counterweight package traces 7021 and along Two counterweight package traces 7021 are moved up and down, the second counterweight component 702 be located at the first counterweight component 701 top and with the first weight Gap 703 is formed between code character part 222.It is noted that the second counterweight component 702 can be located at the first counterweight group The surface of part 701, can also stagger a certain distance, but be the need to ensure that the first counterweight component 701 along the first counterweight component Guide rail 7011 can be leaned when moving up to the second counterweight component 702.In the present embodiment, also pacify in the fixed plate 711 Equipped with two spacer blocks 713, a spacer block 713 is connected between two groups of adjacent counterweight components 70, the spacer block 713 is located at first Between the counterweight package traces 7021 of counterweight package traces 7011 and second so that the first counterweight package traces 7011 and the second counterweight The installation of package traces 7021 is more firm.When the pressing force needed for solar cell module is not above the elasticity of main pressing piece 72 During power, main pressing piece 72 elasticity in the range of elastic force presses lid 2, when the pressing force needed for solar cell module exceedes master During the elastic force of pressing piece 72, then main pressing piece 72 leans the first counterweight component 701 upwards, then now the first counterweight component 701 Work, when the pressing force needed for solar cell module exceedes the gravity sum of the main counterweight component 701 of pressing piece 72 and first When, the main counterweight component 701 of pressing piece 72 and first moves up the distance in the gap 703 along the first counterweight package traces 7011 And continue up and lean the second counterweight component 702, then now the second counterweight component 702 works.
As shown in FIG. 13 to 15, specifically, first counterweight 7014, the second counterweight 7024 are used to be main pressing piece 72 carry out counterweights so that main pressing piece 72 can press pressing force main pressing piece 72 elastic force and the first counterweight 7014, the Solar cell module in the sphere of gravity of two counterweights 7024, first counterweight 7014, the second counterweight 7024 are a set pattern The counterweight of lattice series, can make, it would however also be possible to employ standard test weight according to the need for user, in the present embodiment, and described first Counterweight 7014, the second counterweight 7024 are in rectangular-shape, are easy to be fixed on the first counterweight mounting seat 7013, the installation of the second counterweight respectively On seat 7023, first counterweight 7014, the second counterweight 7024 are gram group counterweight, can also be kilogram group counterweight, the rule of counterweight Lattice are determined according to the solar cell module of required pressing, are selected according to the need for user.First counterweight Sliding block 7012, the length of the second counterweight sliding block 7022 are respectively smaller than the first counterweight package traces 7011, the second counterweight component The length of guide rail 7021, the first counterweight sliding block 7012, the second counterweight sliding block 7022 are in the first counterweight package traces 7011, the second weight The stroke of code package traces 7021 can be closed according to the structure of press component and the solar cell module of required pressing Reason is determined.The first counterweight mounting seat 7013, the second counterweight mounting seat 7023 cross section it is L-shaped, its outside with the first weight Code sliding block 7012, the second counterweight sliding block 7022 are connected, and its inner side is used to install the first counterweight 7014, the second counterweight 7024, can With understanding, the first, second counterweight mounting seat is not limited to the structure of the present embodiment, as long as counterweight cunning can be connected effectively The structure type of block and installation counterweight can be used in the present invention, such as described counterweight mounting seat and counterweight sliding block can also be integrated Set.
Refering to Fig. 1, Figure 14 and Figure 15, in the present invention, the main pressing piece 72 is used for the upper lid 2 of elasticity pressing, the master Pressing piece 72 includes threaded coupling sleeve 721, connecting rod 722, spring 723 and main press head 724, the threaded coupling sleeve 721 are threadedly coupled with the first counterweight mounting seat 7013, in the present embodiment, and the threaded coupling sleeve 721 includes threaded connection Portion 725 and the sleeve part 726 located at the lower section of threaded joints 725.The connecting rod 722 is installed on the spiral shell with can moving up and down In line branch sleeve 721, threaded coupling sleeve 721 is exposed in its upper end, and threaded coupling sleeve 721 is exposed in its lower end;The spring 723 are sheathed on the connecting rod 722, and the upper end of spring 723 leans the inwall of sleeve part 726, the lower end connection connecting rod of spring 723 722, in the present embodiment, step 727 is correspondingly provided with connecting rod 722, the lower end of the spring 723 is resisted against on step 727. The main press head 724 is fixed on the lower end of the connecting rod.By the main pressing piece 72 of said structure, when the band of Z axis moving parts 9 When dynamic press component 7 presses down on lid 2, the main upper lid 2 of the contact of press head 724 is simultaneously pushed, main press head 724 and connecting rod 722 to Upper compression spring 723, the now application of spring 723 spring force is on connecting rod 722 and main press head 724;Make winner's pressing piece 72 can With solar cell module of the pressing force in the range of elastic force needed for elasticity pressing.The spring can be according to required pressing Selected and made the need for solar cell module, with certain stroke and elastic force scope.It is understood that institute Simplest structure can also be used by stating main pressing piece 72, can also only be realized including connecting rod 722 and main press head 724 in pressing The function of lid 2.It is preferred to use the scheme of the present embodiment, by setting spring 723, can realize elastic pressing, effectively Lid 2 in protection, it is to avoid hardness pressing caused may be damaged.Also, because the elastic force of the spring 723 is according to the journey of compression Degree, the size of elastic force is change, thus main pressing piece 72 can be applied with the different pressing forces of lid 2 in certain scope, It is applicable to a variety of solar cell modules of different pressing forces.
When many counterweight press devices work of the present invention, Z axis moving parts 9 drive press component 7 to press down on lid 2, under normal conditions, when the pressing force needed for solar cell module is not above the elastic force of main pressing piece 72, master presses The elasticity in the range of elastic force of casting die 72 presses lid 2, when the pressing force needed for solar cell module exceedes main pressing piece 72 Elastic force when, then main pressing piece 72 leans the first counterweight component 701 upwards, and now the first counterweight component 701 works, and passes through First counterweight component 701 can apply appropriate gravity to main pressing piece 72 so that main pressing piece 72 can be with solar cell The upper lid 2 of pressing force pressing needed for component.In the case where the counterweight of the first selected counterweight 7014 is inadequate, that is, work as solar-electricity When pressing force needed for the component of pond is more than the pressing force of the main counterweight 7014 of pressing piece 72 and first, main pressing piece 72 leans the upwards One counterweight component 701 simultaneously moves up certain gap together with the first counterweight component 701 along the first counterweight package traces 7011 703, the second counterweight component 702 is then leaned, now the second counterweight component 702 works, by setting first, second counterweight group The mode that part and first, second counterweight component are moved along first, second counterweight package traces can be adapted to various solar-electricities Pond component, and avoid the upper lid 2 of hardness pressing.
In the present invention, in order that the stress of upper lid 2 evenly so that more effectively to solar cell module press. In situations where it is preferred, as shown in Fig. 8 to Figure 13, Figure 16 to Figure 18, press component 7 of the invention also include assistant cylinder 73, The device for fixing screen on headrest 74 being connected with assistant cylinder and the array auxiliary pressing piece being installed on device for fixing screen on headrest 74.It is described auxiliary Cylinder 73 is helped to include assistant cylinder body 731, extend the assistant cylinder axle 732 and drive block of assistant cylinder body 731 733, the assistant cylinder body 731 is fixed on mounting bracket 71, the drive block of the device for fixing screen on headrest 74 and assistant cylinder 73 733 are fixedly connected and drive upper and lower motion by assistant cylinder axle 732.In the present embodiment, the assistant cylinder body 731 is consolidated Due in fixed plate 711 and positioned at the top of fixed block 712, assistant cylinder axle 732 is through fixed block 712 with being located at fixed block The drive block 733 of 712 lower sections is fixedly connected, and the device for fixing screen on headrest 74 is fixedly connected with the drive block 733 of assistant cylinder 73, by This, when assistant cylinder 73 works, assistant cylinder body 731 gives the atmospheric pressure of assistant cylinder axle 732, and assistant cylinder axle 732 has There is certain stroke, drive the upper and lower motion of device for fixing screen on headrest 74 so that be installed on the auxiliary pressing piece 75 on device for fixing screen on headrest 74 Press down on lid 2.
In the present embodiment, refering to Figure 18, the auxiliary pressing piece 75 include sleeve 751, connecting rod 752, spring 753 with And auxiliary press head 754, the sleeve 751 is fixed on device for fixing screen on headrest 74, and the connecting rod 752 is installed on the sleeve 751 In and expose the lower end of the sleeve 751, the spring 753 is sheathed in the connecting rod 752 and positioned at the sleeve 751 Interior, in the present embodiment, the upper end of the spring 753 leans the inwall of sleeve 751, and the lower end of spring 753 is connected bar 752;The auxiliary press head 754 is fixed on the lower end of the connecting rod 752.By said structure, when assistant cylinder axle 732 drives Device for fixing screen on headrest 74 and auxiliary pressing piece 75 are moved down, the upper lid 2 of the auxiliary press head 754 of the lower end of connecting rod 752 pressing and under During pressure, auxiliary press head 754 and the upward compression spring 753 of connecting rod 752, the now application of spring 753 spring force is in connecting rod 752 On;The elasticity of auxiliary pressing piece 75 is allowd to press upper lid 2.The need for the spring 753 can be according to solar cell module Selected and made, with certain stroke and elastic force scope.It is understood that the auxiliary pressing piece 75 can also Using simplest structure, only including connecting rod 752 and auxiliary press head 754, by assistant cylinder 73 with dynamic auxiliary pressing piece 75 Move downward, the function of the upper lid 2 of pressing can also be realized.It is preferred to use the scheme of the present embodiment, by setting spring 753, elastic pressing can be realized, upper lid 2 is effectively protected, it is to avoid damaged caused by hardness pressing is possible.Also, due to described The elastic force of spring 753 is according to the degree of compression, and the size of elastic force is change, thus auxiliary pressing piece 75 can be certain In the range of be applied with the different pressing forces of lid 2, it is adaptable to need the solar cell module of different pressing forces.
In addition, device for fixing screen on headrest 74 also includes being used to adjust the Y of the position of the array auxiliary pressing piece in the Y-axis direction Axle guide 741 and/or for the X-axis guide 742 for the position for adjusting array auxiliary pressing piece in the X-axis direction.Ginseng Figure 16 and Figure 17 is read, in the first embodiment of the present invention, pressing piece is aided in the position of Y direction to adjust the array Put, the device for fixing screen on headrest 74 includes being used to adjust the Y-axis guide of the position of the array auxiliary pressing piece in the Y-axis direction 741, be provided with least one X-axis guide 742, each X-axis guide 742 on the Y-axis guide 741 be fixed with it is several Aid in pressing piece 75, the quantity and structure of the X-axis guide 742 can be according to the portions of the solar cell module of required pressing Position is selected and set.The X-axis guide includes the contiguous block 746 for being used to install array auxiliary pressing piece, described Contiguous block 746 is provided with X-axis guide groove 747, in the present embodiment, by lock screw 756 through the screw on contiguous block 746, The screwed hole set with the upper end of sleeve 751 of the auxiliary pressing piece 75 is threadedly coupled, and auxiliary pressing piece 75 is fixed on into connection On block 746.The Y-axis guide 741 causes array auxiliary fixed on the X-axis guide 742 and X-axis guide 742 to press Casting die can be easy to press not the diverse location of ibid lid 2, with preferably to solar battery group along Y direction adjusting position Part is pressed.As shown in FIG. 16 and 17, the Y-axis guide 741 includes guide pad 743 and on guide pad 743 Y-axis guide groove 744.In the present embodiment, the guide pad 743 is H types guide pad 743, and its front end is provided with two Y-axis guide grooves 744.The auxiliary pressing piece mounting bracket 71 also includes the regulating part 740 that can be moved along X-axis guide groove 747, Y-axis guide groove 744, described During regulating part 740 is arranged in 747 in the Y-axis guide groove 744 and X-axis guide groove and it is directed to block 743 and is connected with contiguous block 746; By along Y-axis guide groove 744 and/or X-axis guide groove slidable adjustment part 740, the contiguous block 746 being connected with regulating part 740 along X-axis and/ Or Y direction movement, it is possible thereby to which adjusting the array being fixed on contiguous block 746 aids in pressing piece in X-axis and/or Y direction Position.As long as it is understood that the Y-axis for the position for adjusting the array auxiliary pressing piece in the Y-axis direction can be realized Guide 741 and the structure of X-axis guide of position of array auxiliary pressing piece is adjusted in the X-axis direction be used equally for this Invention, however it is not limited to the mode of above-mentioned setting guide groove and regulating part 740, but the mode of guide groove and regulating part 740 is set, regulation Facilitate and structure is simpler so that the more reasonable structure of device for fixing screen on headrest 74, installation and removal are more convenient.
In summary, first, the press component 7 includes mounting bracket 71, array counterweight component 70 and for pressing Several main pressing pieces 72 of lid 2, the mounting bracket is installed on Z axis moving parts, and Z axis moving parts 9 are installed on X-axis exercise group On part 8, by X-axis moving parts 8, Z axis moving parts 9 main pressing piece 72 can be driven to be moved along X-axis, Z-direction, X-axis fortune Dynamic component 8 is used to drive press component 7 to move along the x-axis to be moved at the diverse location of upper lid 2;Pass through the energy of Z axis moving parts 9 Enough upper lids 2 of driving pressing, so as to be pressed by solar energy layer pressing plate 4 to each position of solar cell module. Main pressing piece 72 presses down on lid 2 under the driving of Z axis moving parts 9, due to needed for different solar cell modules Pressing force is different, when the pressing force needed for solar cell module is not above the elastic force of main pressing piece, main pressing piece 72 Elasticity presses lid 2 in the range of elastic force, when the pressing force needed for solar cell module exceedes the elasticity of main pressing piece 72 During power, then counterweight component 70 works, and can apply appropriate gravity to main pressing piece by counterweight component 70 so that main pressing The dynamics that part 72 can press lid 2 in upper lid 2, pressing with the pressing force needed for solar cell module can in certain scope Effectively automatically adjusted, and the precision pressed is high, can be applicable to a variety of solar cells of different pressing forces Component, it is applied widely.Secondly, the press component 7 also includes device for fixing screen on headrest 74, assistant cylinder 73 and is installed on auxiliary The array helped on fixed mount 74 aids in pressing piece, and auxiliary pressing piece 75 is installed on device for fixing screen on headrest 74, and device for fixing screen on headrest 74 is pacified Loaded on mounting bracket 71, auxiliary pressing piece 75 can be driven along X-axis, Z-direction by X-axis moving parts 8, Z axis moving parts 9 Motion;Also, the device for fixing screen on headrest 74 also includes the position for adjusting the array auxiliary pressing piece in the Y-axis direction Y-axis guide 741 and/or for the X-axis guide 742 for the position for adjusting array auxiliary pressing piece in the X-axis direction;Make Pressing piece 75 must be aided in as needed, in X-direction and the further adjusting position of Y direction, the accurate of pressing is improved Property.Again, the main press head 724 and auxiliary press head 754 are made up of colloid, with press it is thin-skinned the characteristics of, can effectively protect Lid 2 in shield.Also, due to main pressing piece 72 and aid in pressing piece 75 to adjust main press head 724 by counterweight component or spring 753 With the pressing force of auxiliary press head 754 so that the pressing of the main upper lid 2 of 754 pairs of press head 724 and auxiliary press head has cushion effect, power Degree is adjustable, can effectively protect lid 2.
In addition, many counterweight press devices 100 may also include Y-axis moving parts (not shown), X-axis moving parts 8 are pacified Loaded on Y-axis moving parts, Y-axis moving parts are used to drive press component to move along Y-axis so that the pressing scope of press component It is wider, the diverse location of the upper lid 2 of pressing is more convenient, so as to be pressed to the diverse location of solar cell module.Y-axis is moved Component also includes drive motor, drive belt and guide rail respectively, similar to above-mentioned X-axis moving parts 8, Z axis moving parts 9 Structure, those skilled in the art combines the principle of the present invention and according to above-mentioned X-axis moving parts 8, Z axis moving parts 9 The concrete function of Y-axis moving parts can be realized.
It is understood that the press component 7 of many counterweight press devices, X-axis moving parts 8, Z axis moving parts 9, And Y-axis moving parts are electrically connected with central control processing unit, the work of these components is controlled by central control processing unit Make, for example:In many counterweight press devices, the X-axis drive motor of X-axis moving parts 8, the Z axis driving horse of Z axis moving parts 9 Electrically connected up to the part such as 94 and assistant cylinder 73 with central control processing unit, central control processing unit controls these portions The action of part, is achieved in the function of many counterweight press devices.Central control processing unit is realized to this by software program The coordination control of a little parts, it is to be understood that as long as existing software control procedure can realize the required control work(of the present invention The present invention can be used equally for.
Above-mentioned solar components laminater is used to realize following laminating methods, the lamination side of solar components of the invention Method is similar to existing laminating method, and the laminating method of solar components laminater of the invention comprises the steps:Step 1st, solar cell module to be laminated is put into lower chambers;
Step 2, vacuumize:The vent valve of upper and lower chamber is closed, the vacuum valve of upper and lower chamber room is opened, first to lower chambers Progress vacuumizes 35S~40S, then vacuumizes 6min~7mi n simultaneously to upper and lower chamber, observes the registration of vacuum meter to work Needed for skill below vacuum, now, lower chambers vacuum reaches -100Kpa;In above-mentioned vacuum, discharge lower chambers Air, it, which is acted on, avoids solar cell module from generating bubble, and upper chamber uses cooperatively to help in exhaust phase and lower chambers Lower chambers are vented.
Step 3, mechanical lamination process:Upper lid is pressed by many counterweight press devices, is laminated by solar energy Component pressurizes to the solar cell module of bottom chamber, while being heated to lower chambers;In this step, main pressing Part 72 can be adjusted in upper lid 2 under the driving of X-axis drive component 8 the need for the pressing position according to needed for solar cell module On position, then main pressing piece 72 lid 2 is pressed down under the driving of Z axis drive component 9, due to different solar-electricities Pressing force needed for the component of pond is different, when the pressing force needed for solar cell module is not above the elastic force of main pressing piece When, main pressing piece 72 elasticity in the range of elastic force presses lid 2, is pressed when the pressing force needed for solar cell module exceedes master During the elastic force of casting die 72, then counterweight component 70 is worked, and appropriate gravity can be applied to main pressing by counterweight component 70 Part 72 so that main pressing piece 72 can press the dynamics of lid 2 in upper lid 2, pressing with the pressing force needed for solar cell module Effectively automatically adjusted in certain scope, so as to make the bubble between solar cell module smoothly arrange Go out, improve the binding ability between the solar cell module after lamination;In situations where it is preferred, in order that the stress of upper lid 2 Evenly, so as to more effectively be pressed to solar cell module, assistant cylinder axle 732 drives the upper and lower fortune of device for fixing screen on headrest 74 It is dynamic so that the auxiliary pressing piece 75 being installed on device for fixing screen on headrest 74 presses down on lid 2, is together pressed with main pressing piece 72 Lid 2, can preferably press lid 2, the bubble between solar cell module is smoothly discharged, and improve the sun after lamination Binding ability between energy battery component.
In a preferred embodiment of the invention, in addition to pneumatic type lamination process:Close in the vacuum valve of upper chamber, opening The vent valve of chamber, upper chamber enters inflated condition;The vent valve of upper chamber is adjusted, the vacuum meter registration of upper chamber is observed, arrives Upper chamber vent valve is closed after up to lamination pressure;Vacuum is kept by lower chambers, upper chamber is deflated, to bottom chamber too Positive energy battery component is pressurizeed, while being heated to lower chambers, the temperature for keeping lower chambers is 140 DEG C of constant temperature, continues one Fixed lamination times, solar cell module is combined together by heating, pressurization.
The present invention pneumatic type lamination process be preferred to use segmented lamination, specifically, in lamination process, it is described on Chamber persistently keeps vacuum, and the deflation course of the upper chamber is deflated to be stage:1) exhaust phase:Upper chamber is deflated to row Air pressure is strong and keeps the drain pressure for a period of time, the bubble between discharge solar cell module;2) pre-pressing stage:Will be upper Chamber continues to be deflated to precompressed pressure and keeps the precompressed pressure for a period of time, and precompressed is carried out to solar cell module;3) layer The pressure stage:Upper chamber is finally deflated to lamination pressure and keeps the lamination pressure to terminate for a period of time to lamination times, will too Positive energy battery pack pressing is together.
In the present embodiment, in 1) exhaust phase:With 18S to 20S deflation time by upper chamber be deflated to pressure for- 50KPA to -60KPA, keeps 50 to 60S;2) lower chambers are deflated to pressure by pre-pressing stage with 18S to 20S deflation time For -28KPA~-30KPA, 2mi n to 3mi n are kept;3) lamination stages:Vent valve is opened completely, lamination times are remained to Terminate.The control of the stage deflation of above-mentioned upper chamber can pass through upper chamber vacuum pressure sensor, upper chamber vacuum solenoid and control Device processed is realized.For example:In exhaust phase, the pressure that upper chamber vacuum solenoid detects upper chamber reaches drain pressure -50KPA To -60KPA, then controller is signaled to, controller control upper chamber vacuum solenoid is closed, stops deflating to upper chamber.Control Controller controls the upper chamber vacuum solenoid to open to after 60S the default retention time 50 in device processed, continues to deflate, until The pressure that upper chamber vacuum solenoid detects upper chamber reaches precompressed pressure -28KPA~-30KPA, and controller controls upper chamber true again Empty closed electromagnetic valve, stops deflating to upper chamber.Said process is automatically controls, it is of course also possible to according to upper chamber vacuum meter Numerical value is shown, it is corresponding to open and close upper chamber vent valve, to be controlled manually.
The present invention is by way of being segmented and deflating, and the bubble between exhaust phase makes solar cell module is (especially Bubble between sheet glass and EVA) slowly discharged from centre to surrounding, by pre-pressing stage, obtain solar cell module To precompressed, laminating operation is then carried out again, is more beneficial for being laminated out qualified product;And use Chinese patent The continuous progressive deflation of CN200910182703 technical scheme, the product big to lamination area is difficult to ensure that glass plate and EVA Between bubble discharge in time, and without the process of pre- briquetting pressure, the properties of product after lamination are poor.
After step 4, lamination times are reached, upper chamber vent valve is closed, upper chamber vacuum valve is opened, simultaneously closes off lower room vacuum Valve, opens lower room vent valve, after lower chambers vacuum returns to atmospheric condition, lid 2 in opening, by the solar battery group after lamination Part takes out, and lamination process terminates, and solar cell module product is made.
In summary, the laminating method of solar components laminater of the invention by set many counterweight press devices come The mechanical lamination to solar cell module is realized, and in situations where it is preferred, also passes through the vacuum to upper and lower vacuum chamber The pneumatic type for controlling to realize component to be laminated is laminated.First by solar cell module, (five layers of raw material are glass, EVA, battery Piece, EVA, TPT) stack gradually and be placed in lower chambers, upper and lower chamber is first vacuumized, then passes through many counterweight press devices Lid 2 in pressing, upper chamber is compressed, and solar energy layer pressing plate produces deformation, and is pointed to the solar cell module of bottom chamber Certain lamination pressure is produced, so as to realize the mechanical lamination to solar cell module product.Vacuum system can also be passed through Upper chamber is segmented and deflated, lower chambers are always maintained at vacuum, in 140 degree of temperature constant state laminateds, by being segmented lamination and constant temperature Mode the bubble between solar cell module is smoothly discharged, by being mechanically laminated, while preferably in combination with pneumatic Formula is laminated, it is possible to increase the binding ability between solar cell module after lamination, and extrusion there is not bubble, bond strength qualified Solar cell module product;And the solar components laminater of the present invention is widely used, and is conducive to existing solar-electricity The development in pond.
In the description of the invention, it is to be understood that term " first ", " second " etc. be only used for describe purpose, without It is understood that to indicate or imply relative importance.In the description of the invention, unless otherwise indicated, " multiple " are meant that two Or two or more.
Although an embodiment of the present invention has been shown and described, it will be understood by those skilled in the art that:Not In the case of departing from the principle and objective of the present invention a variety of change, modification, replacement and modification can be carried out to these embodiments, this The scope of invention is limited by claim and its equivalent.

Claims (6)

1. a kind of solar components laminater of many counterweights, including:Body, it is openable be installed on the body it is upper Lid, the upper lid is cooperatively formed with body sealing is provided with the sun for being used for being laminated solar cell module in chamber, the upper lid Energy laminate, wherein, the lower chambers for accommodating solar cell module, solar energy are formed between solar energy layer pressing plate and body Upper chamber is formed between laminate and upper lid;Characterized in that, the solar components laminater also includes being used to press Many counterweight press devices of lid, many counterweight press devices are installed on the top of lid, including press component, for driving X-axis moving parts, the Z axis moving parts for driving the press component to be moved along Z axis that press component is moved along the x-axis are stated, The press component is installed on the Z axis moving parts, and the Z axis moving parts are installed on X-axis moving parts;
The press component includes mounting bracket, array counterweight component and several main pressing pieces for pressing upper lid, the peace Shelve and be installed on Z axis moving parts, the array counterweight component is fixed on mounting bracket, several main pressing pieces respectively with The array counterweight component is correspondingly arranged and is connected;
Every group of counterweight component includes at least two counterweight components in the array counterweight component, and the counterweight component includes counterweight group Part guide rail, counterweight sliding block, the counterweight mounting seat being fixedly connected with counterweight sliding block and the counterweight being installed in counterweight mounting seat, The counterweight package traces are installed on mounting bracket, and the counterweight sliding block is installed in counterweight package traces and led along counterweight component Rail is moved up and down, and the main pressing piece is fixedly connected with counterweight mounting seat and is located at the lower section of counterweight;The main pressing piece includes Threaded coupling sleeve, connecting rod, spring and main press head;The threaded coupling sleeve is threadedly coupled with counterweight mounting seat;It is described Connecting rod is installed in the threaded coupling sleeve in which can move up and down, and its upper/lower terminal exposes threaded coupling sleeve respectively;Institute Spring housing is stated on the connecting rod, the upper end of spring leans threaded coupling sleeve, the lower end of spring is against connecting rod;The master presses Pressure head is fixed on the lower end of the connecting rod.
2. the solar components laminater of many counterweights according to claim 1, it is characterised in that the press component is also The device for fixing screen on headrest being connected including assistant cylinder, with assistant cylinder and the array auxiliary pressing being installed on device for fixing screen on headrest Part;
The assistant cylinder includes assistant cylinder body, extends the cylinder axis of assistant cylinder body and be connected with cylinder axis Drive block, the assistant cylinder body is fixed on mounting bracket, and the drive block of the device for fixing screen on headrest and assistant cylinder, which is fixed, to be connected Connect and drive upper and lower motion by cylinder axis;
The device for fixing screen on headrest includes being used to adjust the Y-axis guide of the position of the array auxiliary pressing piece in the Y-axis direction And/or at least one the X-axis guide for the position for adjusting the array auxiliary pressing piece in the X-axis direction;
The auxiliary pressing piece includes sleeve, connecting rod, spring and auxiliary press head, and the sleeve is fixed on device for fixing screen on headrest On, the connecting rod can be installed in the sleeve up or down, and the sleeve is exposed in its lower end, and the spring is located at described In connecting rod and in the sleeve, the upper end of spring leans sleeve, and the lower end of spring is connected bar, the auxiliary press head It is fixed on the lower end of the connecting rod.
3. the solar components laminater of many counterweights according to claim 1, it is characterised in that the Z axis exercise group Part includes Z axis movable plate, at least one Z axis guide rail on Z axis movable plate, Z axis drive belt and for driving Z axis to drive The Z axis drive motor of dynamic endless belt motion, wherein, Z axis drive motor is one or two, is connected to Z axis drive belt One end or two ends, press component is installed in Z axis guide rail, and is connected with Z axis drive belt, in Z axis drive motor Driving under, press component is driven by Z axis drive belt, is slided along Z axis guide rail;
The X-axis moving parts include X-axis movable plate, at least one X-axis guide rail on X-axis movable plate, X-axis drive belt And for driving the X-axis drive motor of X-axis drive belt shuttling movement, wherein, X-axis drive motor is one or two, It is connected to one end or two ends of X-axis drive belt, Z axis moving parts and the press component being installed on Z axis moving parts Integral installation is connected with X-axis drive belt in X-axis guide rail, under the driving of X-axis drive motor, Z axis moving parts Driven, slided along X-axis guide rail by X-axis drive belt with press component.
4. the solar components laminater of many counterweights according to claim 1, it is characterised in that the solar components Laminater also includes vacuum system, and the vacuum system includes vavuum pump and the connection for being used to vacuumize upper and lower chamber Upper and lower room is separately installed with upper and lower vacuum line between upper and lower chamber and vavuum pump, the upper and lower vacuum line to put Air valve and upper and lower room vacuum valve;
The vacuum system also includes being also equipped with upper chamber vacuum pressure sensor, upper chamber on controller, the upper vacuum line Vacuum solenoid, upper chamber vacuum solenoid is in series and is combined into one with upper chamber vent valve, upper chamber vacuum pressure sensor, on Room vacuum solenoid is electrically connected with the controller, upper chamber vacuum pressure sensor by the pressure signal transmission of upper chamber to controller, And be turned on and off by controller control upper chamber vacuum solenoid;
Lower room vacuum pressure sensor, lower room vacuum solenoid, lower room vacuum solenoid are also equipped with the lower vacuum line It is in series and is combined into one with lower room vent valve, lower room vacuum pressure sensor, lower room vacuum solenoid and the controller The pressure signal transmission of lower chambers is controlled lower room true by electrical connection, lower room vacuum pressure sensor to controller, and by controller Empty magnetic valve is turned on and off.
5. the solar components laminater of many counterweights according to claim 1, it is characterised in that the upper lid includes the One top board, the second top board, be provided with first top board in upper groove body, second top board provided with insertion this second The lower groove of top board;The solar energy layer pressing plate for sealing is installed between first top board and the second top board, the sun The upper chamber can be formed between laminate and lower groove;
The body includes support, the heating plate that is installed on support and is seal-installed on being used for above heating plate placing The lower platen of solar cell module, the lower chambers are formed between the solar energy layer pressing plate and lower platen.
6. a kind of laminating method of the solar components laminater of many counterweights, it is characterised in that using such as claim 1 to 5 The lamination of solar battery components device of many counterweights described in any one is realized, is comprised the steps:
S1, solar cell module to be laminated is put into lower chambers;
S2, vacuumize:First lower chambers are vacuumized, then upper and lower chamber vacuumized simultaneously;
S3, mechanical lamination process:Many counterweight press devices are pressed upper lid, then by solar energy layer pressing plate to cavity of resorption Indoor solar cell module is pressurizeed, while being heated to lower chambers;
S4, by after lamination solar cell module take out.
CN201510652102.6A 2015-10-03 2015-10-03 The solar components laminater and its laminating method of a kind of many counterweights Expired - Fee Related CN105172305B (en)

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