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Title:
ENCAPSULATION MATERIAL FOR SOLAR CELL ELEMENT
Document Type and Number:
WIPO Patent Application WO/2006/095911
Kind Code:
A1
Abstract:
To provide an encapsulation material for a solar cell element that would not require the use of any organic peroxide, consequently bringing about an improvement in the efficiency in the production of solar cell modules, and would have such excellent transparency, heat resistance and flexibility as will make a reduction in the thickness of solar cell elements adequately possible, and a solar cell module using the encapsulation material. A preferable embodiment is an encapsulation material for a solar cell element comprising a ethylene-polar monomer copolymer having polar monomer unit content of 10-40 wt% and melting point of not lower than 75°C and HAZE of not more than 10% and meeting the condition of -3.0X+125?T ?3.0X+109, wherein T is melting point (°C) and X is polar monomer unit content (mol%).

Inventors:
Nishijima, Koichi (2-5 Yushudai-nishi, Ichihara-shi Chiba, 25, 29901, JP)
Rioux, Bernard (1 Place du Sud, FR-Puteaux, FR)
Application Number:
PCT/JP2006/305071
Publication Date:
September 14, 2006
Filing Date:
March 08, 2006
Export Citation:
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Assignee:
DU PONT-MITSUI POLYCHEMICALS CO., LTD. (5-2 Higashi-Shimbashi 1-chome, Minato-ku Tokyo, 17, 10571, JP)
E.I.DU PONT DE NEMOURS & COMPANY (1007, Market Street Wilmingto, Delaware, 19898, US)
Nishijima, Koichi (2-5 Yushudai-nishi, Ichihara-shi Chiba, 25, 29901, JP)
Rioux, Bernard (1 Place du Sud, FR-Puteaux, FR)
International Classes:
C08F210/02
Attorney, Agent or Firm:
Nakajima, Shigemitsu (Nichiyo Bldg, 11-12 Kanda Mitoshiro-cho, Chiyoda-k, Tokyo 53, 10100, JP)
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Claims:
CLAIMS
1. An encapsulation material for a solar cell element comprising a ethylenepolar monomer copolymer having polar monomer unit content of 10 40% byweight andmeeting the following conditions (a) to (d): (a) melting point (T 0C) of the copolymer (in accordance with JIS K 7121) and a polar monomer unit content (X mole %) of the copolymer satisfy the following formula: 3.0X+125 > T >3.0X+109 (b) Haze of the laminated sample formed by sandwiching a sheet of the copolymer 0.6mm in thickness with two glass sheets shows not more than 10% provided that haze of the laminated two glass sheets only is 0.5: (c) A melting point is not lower than 75 0C. (d) A storage modulus at 150 0C is not lower than 103 Pa.
2. The encapsulation material for a solar cell element according to claim 1 , whereinthe polarmonomer is an unsaturatedcarboxylic acid ester or vinyl acetate.
3. The encapsulation material for a solar cell element according to claim 1 or 2, the ethylenepolar monomer copolymer is manufactured by a tubular method.
4. The encapsulation material for a solar cell element according to any one of claims 1 to 3, wherein at least one of additives selected from the group consisting of silane coupling agents, antioxidants, ultraviolet absorbers and light stabilizers is compounded into the ethylenepolar monomer copolymer.
5. The encapsulation material for a solar cell element according to any one of claims 1 to 4, wherein the encapsulation material is sheetlike.
6. A solar cell module prepared by using the encapsulation material for solar element defined in any one of claims 1 to 5.
Description:
DESCRIPTION

ENCAPSULATION MATERIAL FOR SOLAR CELL ELEMENT

Technical Field

The present invention relates to an encapsulation material for solar cell elements in solar cell modules and solar cell modules using the encapsulation material. More specifically, thepresent invention is concernedwithan encapsulationmaterial for a solar cell element having excellent transparency, heat resistance, flexibility and other properties that makes the formation of solar cell modules easy.

Background Art Hydroelectric power generation, wind power generation and photovoltaic power generation which makes use of inexhaustible natural energy and help reduce carbon dioxide and improve other environmental problems are getting into the limelight. Out of these, the spread of photovoltaic power generation has been making remarkable progress in recent years as the performance of solar cell modules in power generation efficiency and other respects has been making marked improvements while on the other hand their prices have been declining and the national and local governments has been promoting the business of introducing photovoltaic power generation systems for household use.

However, further spread of photovoltaic power generation will require further cost reductions, and to this end research is

being continued night and day to work particularly on the rationalization of solar cell module manufacturing processes and the improvement of power generation efficiency.

A solar cell module is generally a package comprising a solar cell element such material as silicon, gallium-arsenic and copper-iridium-selenium, a top transparent protective material, a bottom protective substrate material and an encapsulation material, in which the solar cell element is protected with the protective materials and they are fixed each other by using the encapsulation material. For this reason, any solar cell encapsulation material is required to have satisfactory transparency so that power generation efficiency will be increased. A solar cell encapsulationmaterial is also required to have heat resistance so that any troubles such as the flow or deformation will not occur even when the temperature rises during the use of the solar cell module . Furthermore, in recent years, as the thickness of solar cell elements is becoming smaller and smaller, encapsulation materials having excellent flexibility are also sought after. Further, silicon cells are the most expensive, but their semiconductor properties basically do not decline. Because of this, there is a need to remove for reuse the silicone cell alone from a solar cell module after the use of the module or when the part of the module breaks down and is replaced with a new one. However, at present, the encapsulation material is crosslinked and consequently it is impossible to remove the encapsulation material even by heating and melting it . For this

reason, encapsulation materials are required to have a function that will make the reuse of the silicon cell possible.

At present, ethylene-vinyl acetate copolymer having a high vinyl acetate content to which an organic peroxide has been compounded is used as the encapsulation materials for the solar cell elements in solar cellmodules for aviewpoint of flexibility, transparency, heat resistance and other properties. For this reason, it has been necessary for making a solar cell module to use a two-step process in which a sheet-like encapsulation material made of an ethylene-vinyl acetate copolymer containing anorganic peroxide is firstprepared andthen a solar cell element is sealed with such sheet thus obtained.

In the step of making the sheet, it has been necessary to mold the sheet at such low temperature that will not cause the decomposition of the organic peroxide and as the result it is impossible to increase the extrusion rate. On top of that, in the step of encapsulating the solar cell element, it has commonly been necessary to carry out cross-linking process over scores of minutes to one hour in an oven at a high temperature at which the organic peroxide is decomposed. Consequently, much time is required to produce a solar cell module, which in turn constitutes a factor in increasing the manufacturing cost. Besides, the encapsulation material thus obtained does not satisfy the need to reuse the solar cell elements as mentioned above .

To improve the efficiency in producing solar cell modules, the applicant of this application has already proposed a

formulation using an ethylene-unsaturated carboxylic acid copolymer or its ionomer having particular properties (Patent reference 2) . According to this proposal, it was possible to provide a solar cell encapsulation material having excellent transparency, heat resistance, adhesion and other properties and making the formation of solar cell modules easy, but it was difficult for those materials shown in specific examples to meet the need for reducing the thickness of solar cell elements due to their high rigidity. Patent reference 1:Japanese Publication SHO 2-407090

Patent reference 2 :Japanese Laid-openApplication 2000-186114

Disclosure of the Invention

[Issues to be solved by the Invention] Under these circumstances, the inventors of the present invention studied those substitute materials that would not require the use of any organic peroxide, consequently bringing about an improvement in the efficiency in the production of solar cell modules, and would have such excellent transparency, heat resistance and flexibility as will make a reduction in the thickness of solar cell elements adequately possible. As a result, the inventors have found that the material described below is suitable as such substitute materials and successfully made the present invention. [Means for solving the issues]

Specifically, the present invention is the encapsulation material for a solar cell element comprising an ethylene-polar

monomer copolymer having a polar monomer content of 10 to 40 wt% which meets the following conditions (a) through (d) :

(a) The melting point (T 0 C) (in accordance with JIS K7121-1987) of the copolymer and the polar monomer unit content (X mol%) should satisfy the following formula: -3.0X+125 > T > -3.0X+109

(b) The haze of the laminated sample formed by sandwiching a sheet of the copolymer 0.6 mm in thickness with two glass sheets should be not more than 10% provided that the haze of laminated two glass sheets only is 0.5%:

(C) The melting point (in accordance with JIS K7121-1987) should be not lower than 75°C.

(d) The storage modulus at 150°C should be not lower than 10 3

Pa. A preferable example of the ethylene-polar monomer copolymer having the properties described above is a copolymer of ethylene and unsaturated carboxylic acid ester or vinyl acetate, particularly suchcopolymer asmanufacturedbythe tubularmethod .

Furthermore, at least one additive selected from the group of silane coupling agents, antioxidants, ultraviolet absorbers and weathering stabilizers is preferablyaddedtothe ethylene-polar monomer copolymer to be used as the encapsulation material. Further the present invention provides a solar cell module prepared by using the aforesaid encapsulation material. [Effects of the invention]

The encapsulation material of the present invention shows excellent heat resistance as well as satisfactory transparency

and flexibility. Because of this, even if the compounding of the organic peroxide is omitted, it is possible to avoid such troubles as the flowor deformation of the encapsulationmaterial even when the temperature rises during the use of the solar cell module, and there is no possibility of impairing appearance of solar cells. Furthermore, since the encapsulation material makes the omission of the use of an organic peroxide possible, it is also possible to increase productivity in the solar cell module manufacturing process sharply and reduce the manufacturing cost of solar cell modules substantially. Moreover, since the encapsulation material also makes the formation of an encapsulation material layer having excellent flexibility possible, it is possible to avoid the trouble of cracking and cope successfully with the need for lessening the thickness of the solar cell element.

Preferred Embodiments of the Invention

The ethylene-polar monomer copolymer used for encapsulation material of the present invention is a copolymer having polar monomer unit content of 10-40% by weight, preferably 15-40% by weight, in particular 20-38% by weight, which meets above conditions (a) to (d) .

As a polar monomer of ethylene-polar monomer copolymer, there can be exemplified one or more kinds selected from the group of unsaturated carboxylic acid esters such as methyl aerylate, ethyl acrylate, isopropyl acrylate, isobutyl aerylate, n-butyl acrylate, isooctyl acrylate, methyl methacrylate, isobutyl

methacrylate, dimethyl maleate; vinyl esters such as vinyl acetate andvinylpropionate; carbonmonoxide and sulfurdioxide.

Among them, a copolymer of ethylene and unsaturated carboxylic acid ester or vinyl acetate is desirable when considering flexibility, transparency, and others. Particularly preferred is ethylene-unsaturated carboxylic acid ester copolymer, especially ethylene-methyl aerylate copolymer.

A copolymer having properties of the following (a) to (d) as the aforesaid ethylene-polar monomer copolymer is used in the present invention.

(a) The melting point (T 0 C) (temperature showing the greatest endothermic peak in differential scanning calorimeter (DSC)) (by 7121 JIS K, 3146 ISO) and a polar monomer unit content (X mole %) of the copolymer satisfy the following formula: -3.0X+125 > T > -3.0X+109 preferably -3.0X+125 ≥ T ≥ -3.0X+112

(b) The haze of laminated sample formed by sandwiching a sheet of the copolymer 0.6 mm in thickness with two glass sheets shows not more than 10%, preferably not more than 6% provided that haze of laminated two glass sheets only is 0.5%: (C) A melting point is not lower than 75 0 C: and (d) A storage modulus at 150 0 C is not lower than 10 3 Pa. The ethylene-polar monomer copolymer having such properties as above can be positioned a random copolymer having moderate ununiformity since it is superior in heat resistance while showing almost equal transparency comparing with an general

copolymer showing good randomness having the same polar monomer unit content.

Such a copolymer can be produced, for example, by multi-stage autoclave method or tubular method in high-pressure radical polymerization .

Especially, tubular method is more preferable because it is easy to obtain the copolymer having above properties . As an example of the manufacturing methods , there can be cited a method described in Japanese Laid-open Patent Application 62-273214 or Japanese Patent 3423308.

As the ethylene-polar monomer copolymer, the copolymer having melt flowratemeasured at 190 0 C under 216Og load (JIS K 7210-1999 , hereinafterreferredas same) of 0. l-20g/10minute, particularly 0.2-1Og /10 minute is preferably used when considering processability, mechanical strength, thermostability in deforming at high temperature, etc.

For example, it is preferable to use the copolymer showing low deviation of glass at slanting test of 60°at 100 0 C when a laminate formed by sandwiching the copolymer between a glass sheet and an aluminum plate is prepared.

Furthermore, the copolymer having JIS A hardness of not more than 90, preferably not more than 80 is preferably used for enabling to decrease the thickness of the solar cell element.

When using the ethylene-polar monomer copolymer as the encapsulation material for a solar cell, other polymers or various additives can be compounded with the copolymer, as required. As such additives, there can be exemplified silane

coupling agents, ultraviolet absorbers, hindered phenol-type or phosphite-type antioxidants, hindered amine-type light stabilizers, light diffusing agents, fire retardants, antitarnish agents, etc. Although the non-σrosslinked encapsulation material is preferable in the present invention, the encapsulation material may be crosslinked with a crosslonling agent, as desired, when higher heat resistance is required. A silane coupling agent is useful to improve adhesive property of the encapsulation material to protective materials or a solar battery element. As examples of the silane coupling agent, there can be cited a compound having a group to be rendered hydrolysis such as an alkoxy group as well as an unsaturated group such as vinyl group, acryloxy group and methacryloxy group; amino group and epoxy group.

Specific examples of the silane coupling agent include N- (β- aminoethyl)-γ-aminopropyl trimethoxysilane, N- (β-aminoethyl) -Y- aminopropyl methyldimethoxysilane, γ-aminopropyl triethoxysilane, γ-glycidoxypropyl trimethoxysilane, γ- methacryloxypropyl trimethoxysilane, etc.

It is desirable for the silane coupling agent to compound about 0.1-5 parts by weight based on 100 parts by weight of ethylene/polar monomer copolymer. As the ultraviolet absorber that can be added to the encapsulation material for a solar cell element of the present invention, various types of agents such as benzophenone-type agents, benzotriazole-type agents, triazine-type agents and

salicylic acid ester-type agents can be cited. As the benzophenone type ultraviolet absorption agent, there can be cited, for example, 2-hydroxy-4-methoxy benzophenone,

2-hydroxy- 4-methoxy-2 ' -carboxy benzophenone, 2-hydroxy-4-octoxy benzophenone, 2-hydroxy-4-n-dodecyloxy benzophenone, 2-hydroxy-4-n-octadecyloxy benzophenone,

2-hydroxy-4-benzyloxy benzophenone, 2-hydroxy-

4-methoxy-5-sulphobenzophenone, 2-hydroxy-5-chloro benzophenone, 2,4-dihydroxy benzophenone, 2,2 '-dihydroxy-4-methoxy benzophenone, 2 , 2 ' -dihydroxy

-4,4' -dimethoxy benzophenone and 2,2' ,4,4' -tetrahydroxy benzophenone. As the benzotriazole-type ultraviolet absorption agent, there can be cited a hydroxyphenyl-substituted benzotriazole compound, for example, 2-(2-hydroxy-5- methylphenyl) benzotriazole,

2-(2-hydroxy-5-t-butylphenyl) benzotriazole,

2-(2-hydroxy-3,5-dimethylphenyl) benzotriazole, 2-(2-methyl-

4-hydroxyphenyl) benzotriazole,

2-(2-hydroxy-3-methyl-5-t-butylphenyl) benzotriazole, 2-(2-hydroxy-3,5-di-t-amylphenyl) benzotriazole,

2-(2-hydroxy-3,5-di-t-butylphenyl) benzotriazole, etc. As the triazine-type ultraviolet absorbers, there can be cited

2- [ 4 , 6-bis ( 2 , 4-dimethylphenyl) -1 , 3 , 5-triazine-2-yl] -5- (octy loxy) phenol and 2-(4,6-diphenyl-l,3,5-triazine 2-yl)- 5-(hexyloxy) phenol.

As the salicylic acid ester, there can be cited phenyl salicylate and p-octyl phenyl salicylate.

A solar cell module can be prepared by fixing a solar cell element with top and bottom protective materials by using the encapsulation material for a solar cell element of the present invention . As such a solar cell module, various types of modules can be exemplified. Such examples include solar cell modules having structure in which encapsulation materials sandwich both sides of solar battery element like upper part transparent protective material/encapsulation material/solar cell element /encapsulationmaterial / lower part protectivematerial; having structure inwhich theupperpart transparentprotectivematerial and the encapsulation material are formed over the solar cell elementprepared on the front surface of the lower part protective substrate, and having structure in which the encapsulation material and the lower part protective material are formed on a solar cell element prepared on the rear surface of the upper part protectivematerial that is, for example, an amorphous solar cell element prepared by sputtering method or the like on a fluororesin-type protective material

As the solar cell element, there can be used various types of solar cell elements such as silicon-based element including single-crystal silicon, multi-crystal silicon, amorphous silicon, and III-V group or II-VI group compound semiconductor-based element including gallium-arsenic, copper-indium-selenium and cadmium-tellurium. As the upper part protective material constituting the solar cell module, glass, acrylic resin, polycarbonate, polyester, fluorine-containing resin, etc. can be cited.

As the lower partprotectivematerial, single- ormuIti-layered protective material of metal, various types of thermoplastic resins, etc. can be cited. For example, single- or multi-layered protective materials of metals such as tin, aluminum and stainless steel, inorganic materials such as glass, polyesters, inorganic material-deposited polyesters, fluorine-containing resins, polyolefins.

A primer can be adapted to such upper part and/or lower part protective materials to raise adhesive property to the encapsulation material.

The encapsulation material for a solar cell element of the present invention is usually used in sheet shape having thickness of around 0.1-1.2mm, preferably 0.1-lmm.

The sheet-like encapsulation material for a solar cell can be produced by a known sheet formingmethod using T-die extruding machine, calendar molding machine, etc.

For example, the encapsulation material can be obtained by dry-blending ethylene-polar monomer copolymer with additives, as required, such as silane coupling agent, ultraviolet absorption agent, antioxidant and light stabilizer, supplying the blend to T-die extruder through its hopper and molding into sheet-like article.

Of course, a part or all of additives can be used as masterbatch at the occasion of such dry blending. In addition, for T-die extrusion and calendar molding, a resin composition obtained by melt blending ethylene-polar monomer copolymer with a part or all of additives using a mono-axial extruder, a bi-axial

extruder, Banbary mixer, a kneader, ect. can be used.

When preparing solar cellmodules , modules having the structure mentioned above can be formed by a conventionally known method that a sheet of the encapsulation material of the present invention is prepared beforehand and pressed at the temperature which encapsulation material melts. In this case, since it is not necessary to compound the organic peroxide to the encapsulation material, sheet formation of the encapsulation material can be conducted at high temperature with high productivity, and further formation of modules can be completed within short time at high temperature because two-step adhesion process is not necessary.

In addition, it is possible to prepare the solar cell module in one step, without doing sheet forming expressly, by adapting a method for laminating the encapsulationmaterial of the present invention with the solar cell element, or the upper or lower part protective material by extrusion coating.

Therefore, when the encapsulation material of the present invention is used, it becomes possible to improve the productivity of the module markedly.

Examples

The present invention is explained in more detail by practical examples as follows. Raw materials used in examples and comparative examples are as follows . (1) Ethylene-methyl acrylate copolymer (EMA-I):

Content of methyl aerylate unit: 30 % by weight (12.2 % by mole) .

Melt flow rate (JIS K7210, 190 0 C, 216Og load) : 3g /10 minute.

(2) Ethylene-methyl acrylate copolymer (EMA-2): Content of methyl acrylate unit: 35 % by weight (15.0 % by mole) .

Melt flow rate (JIS K7210, 190 0 C, 190 0 C, 216Og load): 3g /10 minute.

(3) Ethylene-vinyl acetate copolymer (EVA): Content of vinyl acetate: 25 % by weight (9.8 % by mole). Melt flow rate (JIS K7210, 190 0 C, 190 0 C, 216Og load): 2.5g /10 minute.

(4) Ethylene-ethyl acrylate copolymer (EEA):

Content of ethyl acrylate: 25 % by weight (8.5% by mole). Melt flow rate (JIS K7210, 190 0 C, 190 0 C, 216Og load): 5 g /10 minute.

(5) Silane coupling agent y -(Methacryloxypropyl) trimethoxy silane

(6) UV absorber Cyasorb UV1164 (Product from Cytec Industries)

( 7 ) Photo stabilizer

(a) Tinuvin 622LD (Product from Ciba Geigy)

(b) Sanol LS770 (Product from Ciba Geigy)

( 8 ) Anti-oxidant Irganox 1010 (Product from Ciba Geigy)

[Example 1]

A sheet of 0.6mm thickness of above ethylene-methy aerylate copolymer (EMA-I) with 0.3 wt% of UV absorber, 0.15 wt% of photo stabilizer (a), 0.15 wt% of photo stabilizer (b) and 0.03 wt% of anti-oxidant was prepared at molding temperature of 12O 0 C with a profile extrudingmachine (diameter of screw: 40mm, L/D=26, full flight screw, compression ratio: 2.6).

The obtained sheet was sandwiched between two blue glass sheets of 3mm thickness and laminated with a vacuum laminator at 150 0 C for 15 minutes. Haze of the laminated sample was measured (haze of laminated two glass sheets only is 0.5%).

The ethylene copolymer sheet obtained above was sandwiched between a blue glass sheet 3 mm thick and an aluminum plate 3 mm thick and laminated with a vacuum laminator at 150 0 C for 15 minutes. The laminated sample was slanted to 60° and held in that position at 100 0 C for 500 hours. The condition of the laminated sample that the glass sheet slid to get out of alignment with melt of the sheet was observed.

Further a sheet of 2 mm thickness of the above copolymer was prepared with a press molding machine. The storage modulus at 150 0 C of the sheet was measured.

The obtained sheet was sandwiched between a blue glass sheet of 3mm thickness and a back sheet (white colored polyethylene terephthalate) and laminated with a vacuum laminator at 15O 0 C for 15 minutes.

Yellowness index of the laminated sample was measured, then the samples were exposed under 2 conditions and after aging

yellowness index of the samples was measured again.

The ethylene copolymer sheet obtained above was sandwiched between a blue glass sheet 3 mm thick and an aluminum plate 3 mm thick and laminated with a vacuum laminator at 150 0 C for 15 minutes .

The results are shown in table 1.

[Example 2]

Evaluation was carried out in the same manner as in Example 1 except that above ethylene-methyl acrylate copolymer (EMA-2) was used instead of EMA-I. The results are shown in table 1.

[Comparative example 1]

Evaluation was carried out in the same manner as in Example 1 except that above ethylene-vinyl acetate copolymer (EVA) was used instead of EMA-I. The results are shown in table 1.

[Comparative example 2]

Evaluation was carried out in the same manner as in Example 1 except that the ethylene-acrylic acid ethyl copolymer (EEA) was used instead of EMA-I. The results are shown in table 1. The melting point, the JIS A hardness, haze and the storage modulus were measured under the following conditions.

( 1) Melting point : The melting point was measured in accordance with a method of JIS K-7121-1987 using a DSC device (Product from Du Pont

Instrument Corporation) .

(2) JIS A hardness:

The hardness was measured in accordance with JIS K 7215 (Durometer A type, Product from Toyo Seiki Seisaku-sho, Ltd. ) .

(3) Haze: Haze was evaluated with a haze meter produced by Suga Test Instruments Co., Ltd. in accordance with JIS K 7105.

( 4 ) Storage modulus :

Storage modulus was measured with the following device under the following conditions.

Device:DVE-V4 FT-Rheospectler produced by Ninon Rheology KIKI

Inc.

Conditions: Pulling mode, sheet thickness of 2mm, frequency of 10Hz, amplitude of 2μm, sine wave, programming rate of 3°C/minute and measurement temperature of 150 0 C.

( 5 ) Aging test .

Yellowness index of laminated samples was measured after aging under below conditions.

Heat resistance : 120 deg C x 500 hours Moisture resistance : 85 deg C x 700 hours

Table 1

It is not possible to measure due to the change in sample's shape.