CN208801704U - Solar panel laminate mechanism and solar battery laminating machine - Google Patents
Solar panel laminate mechanism and solar battery laminating machine Download PDFInfo
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- CN208801704U CN208801704U CN201821064401.3U CN201821064401U CN208801704U CN 208801704 U CN208801704 U CN 208801704U CN 201821064401 U CN201821064401 U CN 201821064401U CN 208801704 U CN208801704 U CN 208801704U
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- 230000007246 mechanism Effects 0.000 title claims abstract description 29
- 238000010030 laminating Methods 0.000 title claims abstract description 12
- 238000003475 lamination Methods 0.000 claims abstract description 49
- 238000007789 sealing Methods 0.000 claims abstract description 18
- 230000003014 reinforcing effect Effects 0.000 claims description 78
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 239000003292 glue Substances 0.000 description 9
- 229910000831 Steel Inorganic materials 0.000 description 8
- 239000010959 steel Substances 0.000 description 8
- 230000009471 action Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000008859 change Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000003672 processing method Methods 0.000 description 4
- 230000000284 resting effect Effects 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000008030 elimination Effects 0.000 description 3
- 238000003379 elimination reaction Methods 0.000 description 3
- 239000003351 stiffener Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 239000000741 silica gel Substances 0.000 description 2
- 229910002027 silica gel Inorganic materials 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000002313 adhesive film Substances 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 210000002435 tendon Anatomy 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
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- Photovoltaic Devices (AREA)
Abstract
The utility model discloses a kind of solar panel laminate mechanism and solar battery laminating machines, are related to machinery equipment field.The technical solution mainly used are as follows: solar panel laminate mechanism comprising: rack, upper lamination cavity and laminated cavity；Upper lamination cavity is oppositely arranged with laminated cavity, can constitute the receiving cavity for accommodating solar panel；Compensation adjustment structure, compensation adjustment structure includes the identical first compensation adjustment structure of structure and the second compensation adjustment structure, first compensation adjustment structure and the second compensation adjustment structure are separately positioned on the opposite first side and second side in laminated cavity lower surface, and it is overlapped with rack, for adjusting the seal clearance between the side of laminated cavity and upper lamination cavity side side when laminated cavity and upper lamination cavity fastening vacuumize sealing.Solar panel laminate mechanism provided by the utility model, solves receiving cavity sealing problem, the cost not increased manufacturing facilities.
Description
Technical field
The utility model relates to machinery equipment field more particularly to a kind of solar panel laminate mechanism and solar-electricities
Pond laminating machine.
Background technique
Solar cell panel structure is generally by back plastic version, EVA packaging adhesive film, semiconductor wafer or semiconductive thin film, ripe
Change glass to melt at 140-160 DEG C, and by EVA glue, loads an atmospheric pressure under vacuum conditions and pass through lamination for battery pack
With EVA glue together curing molding, while the hydrogen that EVA glue generates during crosslinking curing is discharged.So solar panel
Laminating machine is solar panel pressure forming, cured core equipment.
During solar panel vacuum pumpin layer is molded, under critical vacuum state, the meeting of laminated resonator top and bottom
The pressure that about 88 tons of each bootstrap loading, in the insufficient situation of laminated resonator steel construction intensity, the top and bottom of laminated resonator can generate larger
Deformation, seriously affect vacuum sealing face, the laminated resonator steel construction that especially current low cost simple processing obtains influences more
It is prominent.It in the prior art, is high-precision by increasing the high-intensitive gusset quantity being arranged in laminated resonator steel construction and intensity, use
The mode of close processing processes the sealing contact surface of laminated resonator, and using high-power vacuum equipment and when controlling the storage of EVA glue
Between solve above-mentioned technical problem.
But during utility model is created, utility model people discovery, there are following technological deficiencies for the prior art:
The high-intensitive gusset quantity of excessive setting will increase the weight and cost of equipment；High-accuracy processing method, powerful vacuum
Equipment and EVA glue resting period, it not only will increase the cost of equipment, also will increase management cost.
Utility model content
In view of this, the utility model embodiment provides a kind of solar panel laminate mechanism comprising:
Rack, upper lamination cavity and laminated cavity；
The upper lamination cavity is oppositely arranged with the laminated cavity, and the upper lamination cavity being capable of the relatively described lower layer
It presses cavity to carry out open and close movement, when the laminated cavity and the upper lamination cavity fastening, can constitute for accommodating the sun
The receiving cavity of energy solar panel；The central region of the lower surface of the laminated cavity connects by the way that reinforcing rib and the rack are fixed
It connects；
Compensation adjustment structure, the compensation adjustment structure include the identical first compensation adjustment structure of structure and the second compensation
Adjustment structure, the first compensation adjustment structure and the second compensation adjustment structure are separately positioned on laminated cavity lower surface
Opposite first side and second side, and overlapped with the rack, in the laminated cavity and the upper laminated resonator
When body fastening vacuumizes sealing, adjust between the side of the laminated cavity and the upper sealing being laminated between cavity side side
Gap.
It the purpose of this utility model and solves its technical problem also following technical measures can be used to further realize.
Optionally, the quantity of the reinforcing rib above-mentioned is multiple, and multiple reinforcing ribs are distributed in the lower layer
The lower surface of cavity is pressed, and the reinforcing rib extends to four side from the third side of the lower surface of the laminated cavity；
Wherein, the third side setting opposite with the four side, and respectively with the first side and
Dual side-edge connection.
Optionally, the quantity of the reinforcing rib above-mentioned is three, respectively the first reinforcing rib, the second reinforcing rib and the
Three reinforcing ribs；
Wherein, first reinforcing rib is located at the lower surface center of the laminated cavity, second reinforcing rib
The two sides of first reinforcing rib are oppositely arranged on the third reinforcing rib.
Optionally, the first compensation adjustment structure above-mentioned includes reinforcing beam, the reinforcing beam and the laminated chamber
The first side of the lower surface of body connects, and the reinforcing beam is provided with tapped through hole, and is threaded with bolt, by screwing spiral shell
Bolt can be such that bolt mutually pushes up with rack to hold；
Second compensation adjustment structure is identical as the structure of the first compensation adjustment structure, and uses identical set-up mode
The second side of the opposite lower surface that the laminated cavity is set.
Optionally, the quantity of the tapped through hole above-mentioned is multiple, and the setting at the tapped through hole interval adds described
On brutal, and the quantity of bolt and the quantity of the tapped through hole match.
Optionally, the length of the length first side of the reinforcing beam above-mentioned is long；
The quantity of the tapped through hole is two, and two tapped through holes are opposite respectively to be arranged in the reinforcing beam
Both ends, and be located at close to the position at the first side both ends.
Optionally, the reinforcing beam above-mentioned is tee girder, and the tee girder is inverted, the vertical beam of the tee girder and it is described under
It is laminated the lower surface connection of cavity, the crossbeam of the tee girder and the rack overlap；
Wherein, the tapped through hole is arranged on the crossbeam of the tee girder.
In order to achieve the above objectives, the utility model also provides the following technical solutions:
A kind of solar battery laminating machine, comprising: solar panel laminate mechanism；
The solar panel laminate mechanism includes:
Rack, upper lamination cavity and laminated cavity；
The upper lamination cavity is oppositely arranged with the laminated cavity, and the upper lamination cavity being capable of the relatively described lower layer
It presses cavity to carry out open and close movement, when the laminated cavity and the upper lamination cavity fastening, can constitute for accommodating the sun
The receiving cavity of energy solar panel；The central region of the lower surface of the laminated cavity connects by the way that reinforcing rib and the rack are fixed
It connects；
Compensation adjustment structure, the compensation adjustment structure include the identical first compensation adjustment structure of structure and the second compensation
Adjustment structure, the first compensation adjustment structure and the second compensation adjustment structure are separately positioned on laminated cavity lower surface
Opposite first side and second side, and overlapped with the rack, in the laminated cavity and the upper laminated resonator
When body fastening vacuumizes sealing, adjust between the side of the laminated cavity and the upper sealing being laminated between cavity side side
Gap.
By above-mentioned technical proposal, the utility model solar panel laminate mechanism and solar battery laminating machine are extremely
It has the advantage that less
Solar panel laminate mechanism provided by the embodiment of the utility model has additional compensation adjustment structure, compensation
The first compensation adjustment structure and the second compensation adjustment structure in adjustment structure, are separately positioned on laminated cavity lower surface
Opposite first side and second side, and overlapped with rack.It is vacuumized in upper lamination cavity and laminated cavity fastening
When, the life active force for vacuumizing production acts on lamination cavity and laminated cavity, and active force causes to be laminated in cavity
It is mutually compressed in the middle part of portion and laminated cavity, so that the side for being laminated cavity is upturned, the side of laminated cavity
The deformation tilted downwards occurs, and causes to be laminated the sealing space generation gap that cavity and laminated cavity are formed, at this time may be used
To adjust the change that laminated cavity side tilts downwards by adjusting the first compensation adjustment structure and the second compensation adjustment structure
Shape, and then the seal clearance being laminated between cavity and laminated cavity is eliminated, make to be laminated between cavity and laminated cavity
The receiving cavity of composition can quickly realize vacuuming action, without increasing excessive stiffener plate, without high-accuracy
Processing method process upper lamination cavity and laminated cavity, more without using powerful vacuum equipment, and then solving
The production cost of equipment is reduced while technical problem；Furthermore it adds after compensation adjustment structure, can lead to when vacuumizing
The first compensation adjustment structure of adjustment and the second compensation adjustment structure are crossed, quickly realizes the elimination in sealing space gap, and then fast
The realization vacuuming action of speed, so without control EVA glue resting period deliberately, increase management cost that will not be additional, after
And it is practical to be more suitable for solar battery laminating machine provided by the embodiment of the utility model.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of solar panel laminate mechanism provided by the embodiment of the utility model；
Fig. 2 is the Section A-A schematic diagram of Fig. 1；
Fig. 3 is enlarged structure schematic diagram at the position F of Fig. 2；
Fig. 4 is the section B-B schematic diagram of Fig. 1.
Specific embodiment
Further to illustrate that the utility model is the technical means and efficacy reaching predetermined purpose of utility model and being taken,
Below in conjunction with attached drawing and preferred embodiment, to according to the utility model proposes solar panel laminate mechanism and solar-electricity
Pond laminating machine, specific embodiment, structure, feature and its effect, detailed description is as follows.In the following description, different
What " embodiment " or " embodiment " referred to is not necessarily the same embodiment.In addition, special characteristic, knot in one or more embodiments
Structure or feature can be combined by any suitable form.
Embodiment one
As shown in Figure 1, Figure 2 and Figure 4, the utility model embodiment one provides a kind of solar panel laminate mechanism,
Comprising: rack 1, upper lamination cavity 2 and laminated cavity 3；The upper lamination cavity 2 is opposite with the laminated cavity 3
Setting, the upper lamination cavity 2 can the laminated cavity 3 progress open and close movement relatively, when the laminated cavity 3 and institute
It states lamination cavity 2 to fasten, the receiving cavity for accommodating solar panel can be constituted；Under the laminated cavity 3
The central region on surface is fixedly connected by reinforcing rib 4 with the rack 1；Compensation adjustment structure, the compensation adjustment structure packet
Include the identical first compensation adjustment structure 5 of structure and the second compensation adjustment structure 6, the first compensation adjustment structure 5 and second
Compensation adjustment structure 6 is separately positioned on the opposite first side and second side in 3 lower surface of laminated cavity, and with it is described
Rack 1 overlaps, for adjusting the lower layer when the laminated cavity 3 vacuumizes sealing with the upper fastening of lamination cavity 2
Press the seal clearance between the side of cavity 3 and upper lamination 2 side of cavity.
Specifically, rack 1 can be any type of frame body for realizing support function, bearing capacity and specific structure
Form can be configured according to specific needs, the intensity that rack 1 needs to have certain, with guarantee will not when by bearing capacity
It deforms, especially for the biggish place of local pressure, can be strengthened using tripod structure；Rack 1 is preferably with steel
Material manufacture.Upper lamination cavity 2 is the structure that lower surface and 3 upper surface of laminated cavity can make up receiving cavity, upper laminated resonator
The structure of body 2 can be configured with reference to structure in the prior art, such as setting in lower surface edge one week of upper lamination cavity 2
Silica gel plate is sealed by the upper surface of silica gel plate and lower layer pressing plate, and the structure size of upper lamination cavity 2 can be according to specific
Use and set.The main part of laminated cavity 3 can be the polishing steel plate with heating oil duct,
Its burnishing surface is upper surface, and heating oil duct is used to carry out heating work, the knot of laminated cavity 3 to being put into the intracorporal object of chamber
Structure size needs are manufactured with upper lamination cavity 2, and laminated cavity 3 needs to be fixed in rack 1, and preferably horizontal consolidates
It is scheduled in rack 1, is fixed with rack 1 by the way that the reinforcing rib 4 of 3 lower surface of laminated cavity is arranged in, reinforcing rib 4 is set
Set is set to the central region of its lower surface, and preferably reinforcing rib 4 is whole poker structure, i.e., the best width with lower surface
Identical, i shaped steel, T-steel or other structures that can be used in reinforcing fixation can be used in reinforcing rib 4；In addition, laminated
Heating efficiency possessed by cavity 3 can will be heated to required temperature, such as 150 degree as the object in cavity.Upper layer
It can be between pressure cavity 2 and laminated cavity 3 in such a way that one end is rotatablely connected, carry out the adjustment of open and close movement, it can also
To be the upper cooperation for being laminated cavity 2 and being opened and closed by vertical upper and lower movement and laminated cavity 3.Compensation adjustment structure, packet
Two parts i.e. the first compensation adjustment structure 5 and the second compensation adjustment structure 6 are included, two compensation adjustment structures are separately positioned on lower layer
The first side and second side for pressing the lower surface of cavity 3 are mainly used for adjusting the stress deformation of laminated cavity 3, can be with
It is that adjustment structure is held on the top being arranged between laminated cavity 3 and rack 1, such as by bolt 52 or pressure applying means,
Power is acted between laminated cavity 3 and rack 1, and then the deformation of laminated cavity 3 is adjusted, so first is mended
The form that is set as that overlapped between adjustment structure 5 and the second compensation adjustment structure 6 and rack 1 is repaid, is held with facilitating by applying top
The mode of power acts between laminated cavity 3 and rack 1, and then is adjusted to the deformation of laminated cavity 3.In addition, with
In the equipment that realization vacuumizes, realize that the device of movement adjustment and relevant electric appliance ancillary equipment can refer to the prior art
It is configured, the present embodiment is not repeating.
Solar panel laminate mechanism provided by the embodiment of the utility model has additional compensation adjustment structure, compensation
The first compensation adjustment structure and the second compensation adjustment structure in adjustment structure, are separately positioned on laminated cavity lower surface
Opposite first side and second side, and overlapped with rack.It is vacuumized in upper lamination cavity and laminated cavity fastening
When, the life active force for vacuumizing production acts on lamination cavity and laminated cavity, and active force causes to be laminated in cavity
It is mutually compressed in the middle part of portion and laminated cavity, so that the side for being laminated cavity is upturned, the side of laminated cavity
The deformation tilted downwards occurs, and causes to be laminated the sealing space generation gap that cavity and laminated cavity are formed, at this time may be used
To adjust the change that laminated cavity side tilts downwards by adjusting the first compensation adjustment structure and the second compensation adjustment structure
Shape, and then the seal clearance being laminated between cavity and laminated cavity is eliminated, make to be laminated between cavity and laminated cavity
The receiving cavity of composition can quickly realize vacuuming action, without increasing excessive stiffener plate, without high-accuracy
Processing method process upper lamination cavity and laminated cavity, more without using powerful vacuum equipment, and then solving
The production cost of equipment is reduced while technical problem；Furthermore it adds after compensation adjustment structure, can lead to when vacuumizing
The first compensation adjustment structure of adjustment and the second compensation adjustment structure are crossed, quickly realizes the elimination in sealing space gap, and then fast
The realization vacuuming action of speed, so without control EVA glue resting period deliberately, increase management cost that will not be additional, after
And it is practical to be more suitable for solar battery laminating machine provided by the embodiment of the utility model.
As shown in Figure 1 and Figure 4, in specific implementation, the quantity of the reinforcing rib 4 is multiple, between multiple reinforcing ribs 4
Every the lower surface for being distributed in the laminated cavity 3, and the reinforcing rib 4 is from the third of the lower surface of the laminated cavity 3
Side extends to four side；Wherein, the third side setting opposite with the four side, and respectively with described
A side is connected with second side.
Specifically, by above-mentioned it is understood that the set-up mode of multiple reinforcing ribs 4 is preferably the set-up mode of parallel interval,
And the shape that laminated cavity 3 is generally rectangular, so reinforcing rib 4 is preferably arranged in parallel with first side and second side, most
The entire lower surface for running through laminated cavity 3 well, i.e., extend to four side from the third side of laminated cavity 3.Add
The quantity of strengthening tendons 4 is can guarantee that laminated cavity 3 will not be because vacuumizing due to stress deformation.Reinforcing rib 4 and laminated chamber
Connection between body 3 is preferably with welding, and the connection between reinforcing rib 4 and rack 1 is preferably also using welding.
As shown in Figure 1 and Figure 4, further, the quantity of the reinforcing rib 4 is three, respectively the first reinforcing rib 4, the
Two reinforcing ribs 4 and third reinforcing rib 4；Wherein, first reinforcing rib 4 is located at the lower surface center of the laminated cavity 3
Position, second reinforcing rib 4 and the third reinforcing rib 4 are oppositely arranged on the two sides of first reinforcing rib 4.
Specifically, reinforcing rib 4 is preferably with i shaped steel, and in view of the effect of reinforcing rib 4 is to guarantee laminated cavity 3
Central region will not deform because of pressure, so by lower surface center be arranged first reinforcing rib 4, and consider
Three reinforcing ribs 4 can be set in influence to reinforcing rib 4 to equipment cost, other two reinforcing rib 4 distinguishes parallel setting and exists
The distance of the two sides of first reinforcing rib 4, interval can be configured according to specific force analysis result.
As shown in Figure 1-Figure 3, in specific implementation, the first compensation adjustment structure 5 includes reinforcing beam 51, the reinforcement
Beam 51 is connect with the first side of the lower surface of the laminated cavity 3, and the reinforcing beam 51 is provided with tapped through hole, and screw thread
It is connected with bolt 52, bolt 52 can be made to hold with 1 phase top of rack by screwing bolt 52；Second compensation adjustment structure 6 with it is described
The structure of first compensation adjustment structure is identical, and using identical set-up mode it is opposite the laminated cavity 3 is set
The second side of lower surface.
Specifically, reinforcing beam 51 is separately positioned at first side and second side, it is preferably flat with above-mentioned reinforcing rib 4
The connection type of row, reinforcing beam 51 and the lower surface of laminated cavity 3, which may be a fixed connection, to be also possible to be bolted, and with
The overlap joint of rack 1, the in this way cavity when the first lamination cavity and the second lamination cavity fastening composition receiving solar panel, go forward side by side
It when row vacuumizes, such as takes out positive sky and reaches 80 Pascals, the active force for acting on lamination cavity 2 at this time leads to lamination cavity
2 side is upturned, and since laminated cavity 3 is under the action of reinforcing rib 4 and vacuum force, first side
It is deformed downwards with second side；At this point it is possible to make the top of bolt 52 hold rack 1 by screwing bolt 52, and then by the top of bolt 52
Holding force acting in opposition makes the first side of laminated cavity 3 in the first side and second side of the lower surface of laminated cavity 3
Restore deformation upwards with second side, it might even be possible to make the upward deformation in the first side of laminated cavity 3 and second side, in turn
The buckling deformation for making up lamination 2 side of cavity makes the receiving cavity for being laminated cavity 2 and the composition of laminated cavity 3 keep close
Envelope, and then can be quickly true in receiving cavity by adjusting the first compensation adjustment structure 5 and the second compensation adjustment structure 6
Reciprocal of duty cycle reaches requirement, such as reaches 80 Pascals, saves the working time of vaccum-pumping equipment, while the gas for generating EVA glue
Quickly discharge avoids the defect that bubble is generated in solar panel.It should be noted that the bolt for applying bearing force
52 need to select high-strength bolt 52, and bolt 52 can be M18 bolt 52, and 1 position of rack held with 52 phase top of bolt is preferably set
It is set to tripod reinforcement structure.
In addition, that is, during screwing bolt 52, can make screwing bolt 52 during specific compensation adjustment
The top of bolt 52 can stop screwing bolt 52 when holding 1 stress of rack, or adjustment bolt 52 is screwed into according to the actual needs
Degree, as long as can be realized lamination cavity 2 and the sealing of laminated cavity 3.Also it is emphasized that the second compensation adjustment structure
6 and first compensation adjustment structure 5 be same structure, and the set-up mode of the two is also identical, thus in the present embodiment text
When describing the first compensation adjustment structure 5 and set-up mode, it can similarly think that the second compensation adjustment structure 6 is also identical knot
Structure and same set-up mode.
Further, the quantity of the tapped through hole is multiple, and the setting at the tapped through hole interval is in the reinforcing beam
On 51, and the quantity of bolt 52 and the quantity of the tapped through hole match.
Specifically, the quantity of tapped through hole can be selected according to the structure size of laminated cavity 3, i.e. selection force effect
The quantity of point, be laminated instantly cavity 3 size it is larger when, i.e. first side and when larger second side length can be arranged more
I.e. a tapped through hole, such as evenly spaced setting 4-6, to guarantee that sufficiently large work can be applied by screwing bolt 52
Firmly and uniform active force, on the first side and second side of 3 lower surface of laminated cavity.
As shown in Figures 2 and 3, in specific implementation, wherein the length of the length of the reinforcing beam 51 first side
Degree length；The quantity of the tapped through hole is two, and two tapped through holes are opposite respectively to be arranged in the reinforcing beam 51
Both ends, and be located at close to the position at the first side both ends.
Specifically, two are held the threaded hole of bolt 52 preferably adjacent to the both ends of first side and close for be arranged to push up
The both ends of second side can be pushed up by screwing bolt 52 hold first side and second side in this way, both make upward deformation,
Compensate the deformation because vacuumizing generation.
As shown in figure 3, in specific implementation, wherein the reinforcing beam 51 is tee girder, the tee girder is inverted, the T shape
The vertical beam of beam is connect with the lower surface of the laminated cavity 3, and the crossbeam of the tee girder and the rack 1 overlap；Wherein, institute
Tapped through hole is stated to be arranged on the crossbeam of the tee girder.
Specifically, reinforcing beam 51 is it is still further preferred that select tee girder, and tapped through hole is arranged on the crossbeam of tee girder, energy
It is enough to be convenient for screwing bolt 52.
Embodiment two
The utility model embodiment two provides a kind of solar panel laminate mechanism comprising: solar panel
Laminate mechanism；As shown in Figure 1, Figure 2 and Figure 3, the solar panel laminate mechanism include: rack 1, upper lamination cavity 2 with
And laminated cavity 3；The upper lamination cavity 2 is oppositely arranged with the laminated cavity 3, and the upper lamination cavity 2 being capable of phase
Open and close movement is carried out to the laminated cavity 3, when the laminated cavity 3 and the upper fastening of lamination cavity 2, can be constituted
For accommodating the receiving cavity of solar panel；The central region of the lower surface of the laminated cavity 3 by reinforcing rib 4 with
The rack 1 is fixedly connected；Compensation adjustment structure, the compensation adjustment structure include the identical first compensation adjustment structure of structure
5 and the second compensation adjustment structure 6, the first compensation adjustment structure 5 and the second compensation adjustment structure 6 be separately positioned on it is described under
It is laminated 3 lower surface of cavity opposite first side and second side, and is overlapped with the rack 1, in the laminated chamber
When body 3 and the upper lamination cavity 2 fastening vacuumize sealing, adjust the laminated cavity 3 side and the upper laminated resonator
Seal clearance between 2 side of body.
Specifically, the solar panel laminate mechanism provided in embodiment two, is referred to a kind of institute of above-described embodiment
The solar panel laminate mechanism stated, this embodiment is not repeated.
Solar panel laminate mechanism provided by the embodiment of the utility model has additional compensation adjustment structure, compensation
The first compensation adjustment structure and the second compensation adjustment structure in adjustment structure, are separately positioned on laminated cavity lower surface
Opposite first side and second side, and overlapped with rack.It is vacuumized in upper lamination cavity and laminated cavity fastening
When, the life active force for vacuumizing production acts on lamination cavity and laminated cavity, and active force causes to be laminated in cavity
It is mutually compressed in the middle part of portion and laminated cavity, so that the side for being laminated cavity is upturned, the side of laminated cavity
The deformation tilted downwards occurs, and causes to be laminated the sealing space generation gap that cavity and laminated cavity are formed, at this time may be used
To adjust the change that laminated cavity side tilts downwards by adjusting the first compensation adjustment structure and the second compensation adjustment structure
Shape, and then the seal clearance being laminated between cavity and laminated cavity is eliminated, make to be laminated between cavity and laminated cavity
The receiving cavity of composition can quickly realize vacuuming action, without increasing excessive stiffener plate, without high-accuracy
Processing method process upper lamination cavity and laminated cavity, more without using powerful vacuum equipment, and then solving
The production cost of equipment is reduced while technical problem；Furthermore it adds after compensation adjustment structure, can lead to when vacuumizing
The first compensation adjustment structure of adjustment and the second compensation adjustment structure are crossed, quickly realizes the elimination in sealing space gap, and then fast
The realization vacuuming action of speed, so without control EVA glue resting period deliberately, increase management cost that will not be additional, after
And it is practical to be more suitable for solar battery laminating machine provided by the embodiment of the utility model.
Above description is only a specific implementation of the present invention, but the protection scope of the utility model is not limited to
In this, anyone skilled in the art within the technical scope disclosed by the utility model, can readily occur in variation
Or replacement, it should be covered within the scope of the utility model.Therefore, the protection scope of the utility model should be with the power
Subject to the protection scope that benefit requires.
Claims (8)
1. a kind of solar panel laminate mechanism, characterized in that it comprises:
Rack, upper lamination cavity and laminated cavity；
The upper lamination cavity is oppositely arranged with the laminated cavity, and the upper lamination cavity being capable of the relatively described laminated chamber
Body carries out open and close movement, when the laminated cavity and the upper lamination cavity fastening, can constitute for accommodating solar-electricity
The receiving cavity of pond plate；The central region of the lower surface of the laminated cavity is fixedly connected by reinforcing rib with the rack；
Compensation adjustment structure, the compensation adjustment structure include the identical first compensation adjustment structure of structure and the second compensation adjustment
It is opposite that structure, the first compensation adjustment structure and the second compensation adjustment structure are separately positioned on laminated cavity lower surface
First side and second side, and overlapped with the rack, in the laminated cavity and the upper lamination cavity button
When conjunction vacuumizes sealing, the seal clearance between the side of the laminated cavity and the upper lamination cavity side side is adjusted.
2. solar panel laminate mechanism according to claim 1, which is characterized in that
The quantity of the reinforcing rib be it is multiple, multiple reinforcing ribs are distributed in the lower surface of the laminated cavity, and
The reinforcing rib extends to four side from the third side of the lower surface of the laminated cavity；
Wherein, the third side setting opposite with the four side, and respectively with the first side and second side
Side connection.
3. solar panel laminate mechanism according to claim 2, which is characterized in that
The quantity of the reinforcing rib is three, respectively the first reinforcing rib, the second reinforcing rib and third reinforcing rib；
Wherein, first reinforcing rib is located at the lower surface center of the laminated cavity, second reinforcing rib and institute
State the two sides that third reinforcing rib is oppositely arranged on first reinforcing rib.
4. solar panel laminate mechanism according to claim 1, which is characterized in that
The first compensation adjustment structure includes reinforcing beam, the first side of the lower surface of the reinforcing beam and the laminated cavity
Side connection, the reinforcing beam is provided with tapped through hole, and is threaded with bolt, can make bolt and rack by screwing bolt
Mutually top is held；
Second compensation adjustment structure is identical as the structure of the first compensation adjustment structure, and opposite using identical set-up mode
The lower surface that the laminated cavity is set second side.
5. solar panel laminate mechanism according to claim 4, which is characterized in that
The quantity of the tapped through hole be it is multiple, the setting at the tapped through hole interval is on the reinforcing beam, and the number of bolt
It measures and matches with the quantity of the tapped through hole.
6. solar panel laminate mechanism according to claim 5, which is characterized in that
The length of the length of the reinforcing beam first side is long；
The quantity of the tapped through hole is two, two tapped through holes opposite two that the reinforcing beam is arranged in respectively
End, and be located at close to the position at the first side both ends.
7. solar panel laminate mechanism according to claim 4, which is characterized in that
The reinforcing beam is tee girder, and the tee girder is inverted, and the lower surface of the vertical beam of the tee girder and the laminated cavity connects
It connects, the crossbeam of the tee girder and the rack overlap；
Wherein, the tapped through hole is arranged on the crossbeam of the tee girder.
8. a kind of solar battery laminating machine characterized by comprising
The solar panel laminate mechanism as described in any in claim 1-7.
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| CN201821064401.3U CN208801704U (en) | 2018-07-01 | 2018-07-01 | Solar panel laminate mechanism and solar battery laminating machine |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108943966A (en) * | 2018-07-01 | 2018-12-07 | 沈阳工学院 | Solar panel laminate mechanism and solar battery laminating machine |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108943966A (en) * | 2018-07-01 | 2018-12-07 | 沈阳工学院 | Solar panel laminate mechanism and solar battery laminating machine |
| CN108943966B (en) * | 2018-07-01 | 2024-05-28 | 沈阳工学院 | Solar panel laminating mechanism and solar panel laminating machine |
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