Summary of the invention
The present invention aims to provide a kind of solar module, to solve the problem that PID phenomenon appears in solar module in prior art.
To achieve these goals, the invention provides a kind of solar module, comprise backsheet layer stacked successively, the first encapsulating material layer, battery lamella, the second encapsulating material layer and glassy layer, second encapsulating material layer comprises encapsulating material layer, lower encapsulating material layer and for stopping that the metal cation of glassy layer enters the barrier layer of battery lamella, and barrier layer is arranged between encapsulating material layer and lower encapsulating material layer.
Further, barrier layer is the polypropylene that polyimides or fusing point are all more than or equal to that the polyethylene of 100 DEG C or fusing point are all more than or equal to 100 DEG C.
Further, the thickness on barrier layer is within the scope of 5 μm ~ 200 μm.
Further, the number of plies on barrier layer is one deck.
Further, the number of plies on barrier layer is multilayer, and the thickness on every layer of barrier layer is more than or equal to 2 μm.
Further, the thickness of upper encapsulating material layer and the thickness sum of lower encapsulating material layer and the ratio of the thickness of the second encapsulating material layer are within the scope of 0.2 ~ 0.6.
Further, battery lamella is monocrystal solar cell, class single crystal battery, polysilicon solar cell or the hetero-junction solar cell based on crystalline silicon.
Further, the first encapsulating material layer, upper encapsulating material layer and lower encapsulating material layer are EVA, PVB, TPU, PO or Inomer.
Further, backsheet layer is glass, steel plate or aluminium sheet.
Apply technical scheme of the present invention, between upper encapsulating material layer and lower encapsulating material layer, barrier layer is set, barrier layer can stop that the metal cation of glassy layer enters into battery lamella, this avoid the surface that metal cation is gathered in battery lamella, the surface of battery lamella is not easily passivated, and then avoid producing PID phenomenon, thus ensure that the output of the normal power of photovoltaic module.
Embodiment
It should be noted that, when not conflicting, the embodiment in the application and the feature in embodiment can combine mutually.Below with reference to the accompanying drawings and describe the present invention in detail in conjunction with the embodiments.
As shown in Figure 1, the solar module of the present embodiment comprises stacked successively backsheet layer 10, first encapsulating material layer 20, battery lamella 30, second encapsulating material layer 40 and glassy layer 50, second encapsulating material layer 40 comprises encapsulating material layer 41, lower encapsulating material layer 43 and for stopping that the metal cation of glassy layer 50 enters the barrier layer 42 of battery lamella 30, and barrier layer 42 is arranged between encapsulating material layer 41 and lower encapsulating material layer 43.
The solar module of application the present embodiment, between upper encapsulating material layer 41 and lower encapsulating material layer 43, barrier layer 42 is set, barrier layer 42 can stop that the metal cation of glassy layer 50 enters into battery lamella 30, this avoid the surface that metal cation is gathered in battery lamella 30, the surface of battery lamella 30 is not easily passivated, and then avoid producing PID phenomenon, thus ensure that the output of the normal power of photovoltaic module.
In the prior art, in order to ensure that the actual power of solar module exports, publication number is that the Chinese patent of CN102864439A discloses a kind of method preparing the antireflective coating with anti-PID effect, and the metal cation of glassy layer in solar module can be hindered to move to silion cell.Publication number is that the Chinese patent of CN102945890A discloses one at crystalline silicon front side of matrix formation SiO
2/ SiN
xthe technique of lamination composite membrane, with realize crystal silicon cell assembly current potential bring out decay qualified.
Similar patent CN102864439A and patent CN102945890A etc. adopt chemical deposition process to prepare the method for MULTIPLE COMPOSITE rete, for the battery production business having ripe production line, on the one hand, increase passivation technology difficulty, affect productive temp and production capacity.On the other hand, need to transform existing equipment, add manufacturing cost to a certain extent.
And the preferred embodiment of the application efficiently solves the problem that technology difficulty is large, manufacturing cost is higher.In a preferred embodiment, successively by stacked to backsheet layer 10, first encapsulating material layer 20, battery lamella 30, second encapsulating material layer 40 and glassy layer 50, lamination after connection convergent belt, obtains the solar module of anti-PID effect after the surrounding frame for installing of solar module.Independently can carry out synchronous with the passivation technology of solar cell for the preparation of second encapsulating material layer 40 with barrier property in preferred embodiment, then by laminating technology, both be encapsulated, which decrease the technology difficulty that solar cell manufactures.While guarantee solar module dependability, do not affect productive temp, can be widely used in actual volume industrial production, effective production control cost.
In the present embodiment, barrier layer 42 is the polypropylene that polyimides or fusing point are all more than or equal to that the polyethylene of 100 DEG C or fusing point are all more than or equal to 100 DEG C.Certainly, barrier layer 42 also can be polyimide derivatives, Kynoar, polyvinylidene fluoride ene derivative, polyacrylonitrile, HPAM Degraded Bacteria, poly-to benzene ethanedioic acid second diester, poly-to benzene ethanedioic acid second diester deriv, polymethyl methacrylate or polymethyl methacrylate derivative.
In the present embodiment, the number of plies on barrier layer 42 is one deck, and the thickness on barrier layer 42 is within the scope of 5 μm ~ 200 μm.Realize the cationic performance of barrier layer 42 barrier metal so further.
In the present embodiment, the number of plies on barrier layer 42 is multilayer, and the thickness on every layer of barrier layer 42 is more than or equal to 2 μm, and the gross thickness of barrier 42 is within the scope of 5 μm ~ 200 μm.Certainly, also encapsulating material layer can be set between adjacent two-layer barrier layer.The cationic performance of barrier layer 42 barrier metal can be realized so better.
In the present embodiment, the thickness of upper encapsulating material layer 41 and the thickness sum of lower encapsulating material layer 43 and the ratio of the thickness of the second encapsulating material layer 40 are within the scope of 0.2 ~ 0.6.The encapsulation of solar module can be ensured like this.
In the present embodiment, battery lamella 30 is monocrystal solar cell, class single crystal battery, polysilicon solar cell or the hetero-junction solar cell based on crystalline silicon.
In the present embodiment, the first encapsulating material layer 20, upper encapsulating material layer 41 and lower encapsulating material layer 43 are EVA(ethylene-vinyl acetate copolymer), PVB(polyvinyl butyral resin), TPU(polyurethane elastomer), PO(thermoplasticity or thermosetting polyolefin) or Inomer(polyethylene-acetic acid esters ionomer).
In the present embodiment, backsheet layer 10 is glass, steel plate, aluminium sheet or fluoropolymer.Fluoropolymer layer comprises PVF(polyvinyl fluoride) layer and PET(PETG) layer, pet layer is arranged between two-layer PVF layer.
The solar module obtained according to above-described embodiment of the application, is exemplified below:
The thickness of example 1: the two EVA layer is 0.5mm, and wherein, the thickness of upper EVA layer and the thickness of lower EVA layer are 0.18mm, and the thickness of polyimide layer is 0.14mm.
The thickness of example 2: the two EVA layer is 0.5mm, and wherein, the thickness of upper EVA layer and the thickness of lower EVA layer are 0.1mm, and the thickness of every strata vinylidene is 0.1mm, also can arrange EVA layer between adjacent two layers Kynoar.
The thickness of example 3: the two EVA layer is 0.5mm, and wherein, the thickness of upper EVA layer and the thickness of lower EVA layer are 0.2mm, and the thickness that fusing point is all more than or equal to the polyethylene layer of 100 DEG C is 0.1mm.
The thickness of example 4: the two EVA layer is 0.5mm, and wherein, the thickness of upper EVA layer is 0.15mm, and the thickness of lower EVA layer is 0.18mm, and the thickness that fusing point is all more than or equal to the polypropylene layer of 100 DEG C is 0.15mm.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, for a person skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.